18 January 2006
Apparently this document is titled "ICBM Security Classification Guide (SCG), 30 Sep 97." The Google HTML of the original DOC had no title or classification marking, but one citation states the document is classified but does not give the level classification.
The document and two related changes were discovered when searching for the term "TOP SECRET/SIOP/ESI." Original documents have been removed and only Google's HTMLs remain.
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1146
DEPARTMENT OF THE AIR FORCE
HEADQUARTERS OGDEN AIR LOGISTICS CENTER
HILL AIR FORCE BASE, UTAH 84056-5609
FOREWORD
Description: The purpose of this security classification guide is to
provide the basis for assigning the degree of security protection for
information, regardless of form, concerning the Minuteman and Peacekeeper
weapon systems. The Minuteman and Peacekeeper weapon systems include
the Minuteman and Peacekeeper Intercontinental Ballistic Missiles (ICBMs),
launch facilities (LFs), missile alert facilities (MAFs), missile support
bases (MSBs), support equipment, test equipment/facilities and
Minuteman/Peacekeeper operational codes. This Guide should be used
in conjunction with the MK11, MK 12, MK 12A, MK 21 Guides.
AUTHORITY: DoD 5200.1-R/AFI 31-401, Information Security Program Management
and Executive order 12958, Classified National Security Information.
OFFICE OF PRIMARY RESPONSIBILITY: ICBM System Program Office, Ogden
Air Logistics Center (OO-ALC/LM)
ORIGINAL TOP SECRET CLASSIFICATION AUTHORITY: Commander, Ogden Air
Logistics Center
ORIGINATING OFFICIAL:
THOMAS W. TAIT
Deputy Program Director
ICBM Systems Program Office
COORDINATING OFFICIAL: APPROVING OFFICIAL:
TIMOTHY G. HARDY, Lt Col, USAF RICHARD H. ROELLIG, Major General, USAF
Commander, 75th Security Forces Squadron Commander
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Table of Contents
Section Page
I General Instructions 1
II Administrative Details 3
III Performance Data 5
IV Definitions 9
V Distribution List 13
Attachment I (Minuteman)
I Funding, Procurement and Production 1
II Hardware Classification 3
III Propulsion Subsystems 25
IV Missile Guidance Set (MGS) Subsystem 27
V Reentry Systems (RS) 29
VI Improved Minuteman Physical Security System (IMPSS) Security Auxiliary 37
VII Launch Facility Personnel Access Auxiliary System 41
VIII Airborne Launch Control System (ALCS) Auxiliary System 43
IX Communications - Electronics 45
X Testing Program 47
XI Operational Ground Equipment (OGE) 55
XII Facilities 57
XIII Operational Data 59
XIV Nuclear Hardness & Survivability (NH&S) 67
XV System Safety Fault Tree Analysis Results 79
XVI Unauthorized Launch and Launch Action Studies 81
XVII Minuteman II PEN AIDS MK21/MK21A PEN AIDS 83
XVIII Minuteman III PEN AIDS (MK12/MK12A PEN AIDS) 87
Part A - Complete PEN AIDS System 87
Part B - Chaff Subsystem 89
Part C - Decoy Subsystem 93
XIX Software and Data 97
XX Rapid Message Processing 105
Attachment 2 (Peacekeeper)
I Funding, Procurement and Production 1
II Missile Systems 3
III Propulsion Subsystems 7
IV Guidance and Control Subsystems 11
V Basing 15
VI Communications-Electronics-Status Authentication 19
VII Operational Support Equipment (OSE) 23
VIII Operational/Mission Planning Software 25
IX Improved Minuteman Physical Security System (IMPSS) Security Auxiliary System 27
X Nuclear Hardness & Survivability (NH&S) 31
XI Airborne Launch Control System (ALCS) Auxiliary System 43
XII Testing Program 47
XIII Operational Data 55
XIV Unauthorized Launch and Launch Action Studies 61
XV System Safety Fault Tree Analysis Results 63
XVI Hardware Classification 65
SECTION I
GENERAL INSTRUCTIONS
1. PURPOSE: This Guide identifies information developed during various phases of the development, production, deployment and subsequent maintenance phases of the Minuteman and Peacekeeper weapon systems requiring protection in the interest of national security.
2. OFFICE OF PRIMARY RESPONSIBILITY (OPR): This Guide is issued by OO-ALC/LM. Classification management of this Guide is the responsibility of 75 SFS/SFA. Inquiries concerning content or interpretation of this Guide should be addressed to:
OO-ALC/LMDM 75 SFS/SFAI
6014 Dogwood Ave 6010 Gum Lane
Hill AFB UT
84056-5816 Hill AFB UT 84056-5825
DSN 777-3015 DSN 777-7811
COMM (801)
777-3015 COMM (801) 777-7811
3. CLASSIFICATION RECOMMENDATIONS: Send completely documented and justified recommendations for change through appropriate channels to the OPR if the security classifications in this Guide impose impractical requirements, or if operational conditions, technological changes in the state-of-the-art, or any other contributory factors indicate a need for changes. Pending final decision, handle and protect the items of information involved at the highest of the present or recommended classifications. Users of this Guide are encouraged to assist in improving and maintaining the currency and adequacy of this Guide.
4. APPLICATION, REPRODUCTIONS, AND DISSEMINATION:
a. Specified groups involved with Minuteman and Peacekeeper weapon systems, including industrial activities may make reproductions and extracts or selections of portions of this Guide.
b. Distribution of this Guide includes those offices specified in DOD 5200.1-R and other interested Government agencies and contractor facilities.
c. All agencies and offices requiring this Guide will be on an official distribution list whether it be primary distribution from this office or secondary distribution from the base or unit focal point.
5. "FOR OFFICIAL USE ONLY" (FOUO): For Official Use Only (FOUO) is not a security classification. However, handle, protect, and dispose of FOUO information according to AFI 37-131, Freedom of Information Act Program or the applicable industrial security guideline, DOD 5220.22-M, National Industrial Security Program Operating Manual.
6. MANUFACTURE, TEST, AND ASSEMBLY: During manufacture, test, and assembly process, the classification assigned by this Guide applies at the earliest point whenever design, performance, and/or other classified characteristics can be derived from or traced to the system(s) identification herein.
7. DISASSEMBLY AND REPAIR: During disassembly and repair, the classification assigned by this Guide no longer applies at the earliest point where design, performance or other classified characteristics can no longer be derived from or traced to the system(s) identified herein.
8. TEMPEST REQUIREMENTS: TEMPEST requirements must be considered whenever classified automated data processing (ADP) will occur. ADP refers to any electronic or electromechanical equipment which might process classified information.
ADMINISTRATIVE DETAILS
1. PUBLIC RELEASE: The fact that this Guide shows certain details of information as unclassified does not permit automatic public release of them. Send proposed public disclosures of unclassified information regarding MM ICBMs to OO-ALC/PA, 7981 Georgia Street, Hill AFB, UT 84056-5824 for review before the date the proposer needs them for release.
a. The term "information" applies, but is not limited to, articles, speeches, photographs, brochures, advertisements, displays, and presentations, on any phase of the MM or PK weapon system.
b. Defense contractors and other agencies must screen all information they submit for determination of releasability to ensure it is both unclassified and technically accurate. The letter of transmittal must certify this view. Copies of the material may not be released outside official channels until the review process is complete. If you find information during the review process that you suspect is classified, notify all holders of the document the degree of protection required. When doubt exists concerning the classified status of a proposed release pertaining to this program, OO-ALC/LM makes the final decision. The material submitted for review must include a valid suspense date, if applicable.
c. Only information that has been reviewed and certified for public release may be released. Submit information developed after initial approval for public release for review and further processing as outlined in a. and b.
d. Material which requires an export license may not be entered into security review channels for public release approval to circumvent the licensing requirements of the Departments of State and Commerce.
e. Obtain approval for planned or contemplated visits of public media representatives from OO-ALC/LM and OO-ALC/PA.
2. RELEASE OF CLASSIFIED INFORMATION TO FOREIGN GOVERNMENTS OR THEIR REPRESENTATIVES: Any military activity or defense contractor receiving a request from a foreign government or representative thereof for classified information pertaining to the MM AND PK weapon system must send the request to OO-ALC/FMM/FDPO, Hill AFB, UT 84056. Contractors who wish to honor such requests rather than send them to the Foreign Disclosure Office, must apply for an export license according to the International Traffic in Arms Regulation (ITAR) and notify the military of their intent to apply for such license.
3. RELEASE OF UNCLASSIFIED TECHNICAL INFORMATION (NOT APPROVED FOR PUBLIC RELEASE) TO U.S. CITIZENS OR FOREIGN NATIONALS RESIDING IN A FOREIGN COUNTRY: Any defense contractor must either obtain the approval from the cognizant military activity under the ITAR or apply for an export license to the Department of State under the ITAR and notify the military of their intent to apply for such license. Material which requires an export license may not be entered into security review channels for public release approval in order to circumvent the license requirements of the Departments of State or Commerce.
4. This publication of the ICBM Security Classification Guides incorporates the changes mandated in Executive Order 12958. The following information is provided as a quick reference as to reasons for classification and declassification exemptions.
 To be eligible for classification, information must fall within one or more of the categories of information listed in Section 1.5 of the Order. These reasons are identified in the guide as 1.5.a, 1.5.b, etc.
a. Military plans, weapons systems, or operations.
b. Foreign government information.
c. Intelligence activities (including special activities), intelligence sources or methods, or cryptology.
d. Foreign relations or foreign activities of the United States, including confidential sources.
e. Scientific, technological, or economic matters relating to the national security.
f. United States Government programs for safeguarding nuclear materials or facilities.
g. Vulnerabilities or capabilities of systems, installations, projects or plans relating to the national security.
 All information must be declassified or reevaluated within 10 years unless it meets one or more of the criteria established by the Order. These exemptions are identified in the guide as X1, X2, etc.
X1. Reveal an intelligence source, method or activity, or a cryptologic system or activity.
X2. Reveal information that would assist in the development or use of weapons of mass destruction.
X3. Reveal information that would impair the development or use of technology within a United States weapons system.
X4. Reveal United States military plans or national security emergency preparedness plans.
X5. Reveal foreign government information.
X6. Damage relations between the United States and a foreign government, reveal a confidential source, or seriously undermine diplomatic activities that are reasonably expected to be ongoing for a period longer than 10 years.
X7. Impair the ability of responsible United States Government officials to protect the President, the Vice President, and other individuals for whom protection services, in the interest of national security, are authorized.
X8. Violate a statute, treaty, or international agreement.
PERFORMANCE DATA
1. The purpose of this section is to establish the philosophy of the classification of test data, raw and processed, and operational data. Precise distinctions between unclassified and classified data or between data at various levels of classification cannot always be achieved. Often, the decision as to proper classification of data depends upon the context in which the data is viewed or to the extent to which the source and nature of the data is apparent or, particularly in the case of raw data, on the availability of information on the format or storage or calibration conventions which are required in order to understand the information in the data. Keeping the above factors in mind, judgment should be used in assigning classification.
a. Data may be derived from flight test of components or the entire system. The components flown may be operationally or experimentally configured. The data may directly originate from:
(1) Instruments on the components flown: accelerometers, temperature sensors, ablation gauges,Âetc.
(2) Off-board instrumentation: radars, cameras, optical sensors, radiometers, splash detectors, etc.
b. Data may be derived from ground tests of components of the system. The configuration may be either operational or experimental. The data may originate from a variety of sources.
c. Data may originate from theoretical studies, in the form of quantitative predictions or interpretations of system component performance under specified conditions.
2. DATA DIFFERENTIATION:
a. A collection of data is known as a record regardless of the physical form in which the data appears. For the purposes of this Guide, it is proper to distinguish three types of data records.
(1) Raw data record. The primary characteristics of a raw data record are that it contains data as recorded by a sensor (often in real time) and no significant effort has been made to reduce, edit, select or interpret the data. Raw data records commonly appear in one of the following forms:
Magnetic tapes
Decks of computer cards
Computer printouts (listings)
Manuscript scratch sheets
Oscillograph records
Rough operator logs
Photographic displays:
Ballistic camera plates (or prints)
Radar display films (RTI, A-Scope, etc)
Similar display films of other instruments, etc.
Raw data records generally have some, but a minimum of, identification and calibration information. They have few or no annotations or comments relating to the intrinsic difference of the data but typically have comments on the operating conditions of the instrument generating the data (shutter speed, pointing angles, waveform transmitted, etc.) or on the operating condition of the instrument recording the data (framing rate, sweep speed, format conventions, etc.).
(2) Processed data record. A processed data record generally appears in one of two forms:
(a) As a raw data record (or portion of one) plus commentary or annotations revealing the identity and significance of the record and of the information contained to an extent which could not have been derived from the raw data record itself. Examples are:
An annotated RTI film with altitude markings and body identification.
An annotated ballistic or spectral camera print.
A computer listing of the contents of a (raw data) magnetic tape with the addition of revealing column headings and test identification.
(b) Information computed from a raw data record and presented in a revealing and intelligible format. Examples are:
A plot of missile signature versus altitude with identification of plotted parameters, their units and their source.
A computer printout of the ballistic coefficient of a reentry body, identified as such.
In the first case above, the change from raw to processed data came about through the addition of information to the raw data record. In the second case, the processed record is physically different from a raw data record. In both cases, however, there is enough information for a casual reader to understand the meaning of the presentation.
The essence of a processed data record is that it displays significantly more information than is evident in the raw data record from which it was derived. It may be said a raw data record contains data and a processed data record contains information. This information tends to be narrow in scope and restricted in its application to the original data record.
(3) Analyzed data record. Analyzed data records consist of presentations of processed data accompanied by textual material which comments in detail on the significance of the information shown. Conclusions are drawn or implied. The reader's attention is directed to peculiarities or to characteristic phenomena; features noted are often described as being "expected," "typical" or "normal," or conversely as being "unusual," "not previously seen," etc.
Commonly, the textual material is based on a set of raw or processed data more extensive than presented in the analysis. Conclusions are listed which are believed to be valid and of practical importance across a variety of system conditions and, in particular, across a variety of possible future missile flights. Little or nothing is required of the reader in any way of further calculation or interpretation.
Analyzed data tends to have overtones of practical application in that the behavior of operational configurations of the RS is discussed or suggested.
b. Classification of data records
(1) Raw data record. In general, a raw data record is classified according to the level of information it might reasonably disclose to a reader. Refer to appropriate portions of this Guide to determine those levels. However, if:
(a) The record bears no identification which associates it with a specific system either directly* or inferentially**, and if
(b) The record does not disclose information which conflicts with other provisions of this Guide, then the raw data is UNCLASSIFIED.
NOTE: Even if a raw data record contains identification to the MK 12 RS but other information is necessary to draw meaningful conclusions from the record, then the record is UNCLASSIFIED.
(2) Processed data record. Specific provisions elsewhere in this Guide (primarily, but not solely, in Sections V, VI, VII, XIII and XVI) establish the classification of processed data when it is identified as being related to the MM weapon system, or to some component thereof.
(3) Analyzed data record. Analyzed data records are, by their nature, difficult or impossible to strip of identity. Hence, they are classified at the level of the most highly classified information disclosed as determined by this Guide. If, however, the analyzed data record discloses significant operational characteristics of AVE (RS, G&C, missile), consideration must be given to classifying the analyzed data TOP SECRET even if no portion of the record is individually TOP SECRET. In particular, if this or any analyzed data record discloses a system feature which provides a means of discrimination between decoys and RVs or between RV-bearing chaff clouds and non-RV-bearing chaff clouds, it must be classified TOP SECRET-FRD. If any analyzed data record represents vulnerability to the MM III or PK weapon systems, it must be classified TOP SECRET.
For example, the level of classification may in part depend upon whether the record is based on relating to the RS in an operational configuration or to the RS in experimental configuration. Other matters equal, records based on operational configurations are more likely TOP SECRET candidates. It is emphasized, however, that if the analysis of experimentally configured RS components has a direct and immediate application to the performance of an operationally configured RS, there may be justification for classifying the analyzed data record based on the experimental configuration as TOP SECRET.
3. OPERATIONAL DATA:
Operational data includes that data accumulated during normal operation of
the weapon system recorded by the Expanded Missile Data Analysis System (EMDAS)
and consisting of Line Replaceable Unit (LRU) failure, system status and
Inertial Measuring Unit (I) Performance Data (IPD). While these data
elements may lead to classified data, they, in themselves, under the definitions
provided by this Guide, do not provide information for the derivation of
reliability and accuracy.
a. LRU failure and system status data
LRU failure and system status data provides information that supports the determination of system and subsystem reliability. Since this data provides only some of the factors required, it does not provide specified interval or stated condition; it is considered UNCLASSIFIED unless specifically classified in accordance with other sections of this Guide.
b. IPD
IPD originates in the MGS as a result of normal alert operations. These data express the ground performance of the inertial instruments and airborne computer computations relating to that performance. While these data are used to measure stability and predict long term performance and are related to guidance accuracy, it is not sufficient to predict weapon system accuracy. The official alert rate cannot be derived from IPD even though the operational status of some key components of the weapon system can be.
SECTION IV
DEFINITIONS
a. Access:
(1) Physical access: The ability to manipulate an item either in person or remotely. This implies capability to sample material, exchange, touch or conduct unauthorized tests.
(2) Visual access: Access using sense of sight of the hardware. Includes photos, drawings, sketches videos.
b. Assembly: The first major subdivision of a component.
c. Atomic weapon: An atomic weapon as defined in Public Law 708, 83rd Congress, Section 11d, is any device utilizing atomic energy, exclusive of the means of transporting or propelling the device (where such means is a separable or divisible part of the device), the principal purpose of which is for use as or for development of a weapon, weapon prototype or weapon test device. See Reentry Vehicle (RV) Guides.
d. Auxiliary system: A separate function associated with the missile weapon system but not part of the missile itself (e.g., launch facility personnel access auxiliary system).
e. Component: The first major subdivision of a subsystem; e.g., the computer is a component of the guidance subsystem.
f. Computer memory security check (CMSC): A nonlinear compilation of memory content resulting in a characteristic number.
g. Communications Security (COMSEC): COMSEC is a process designed to protect any and all information that may be of possible intelligence value. A designation or marking applied to all information concerning COMSEC exclusive of that designated CONTROLLED COMSEC ITEM or CRYPTO (former designation still in use).
(1) CONTROLLED COMSEC ITEM: A designation or marking which identifies information exclusive of operational keying material which contains a cryptographic logic or which performs a critical COMSEC function.
(2) CRYPTO: A designation or marking which identifies classified keying material and which indicates that the material requires special consideration with respect to access, storage and handling. The ground rules for "CRYPTO" were changed a number of years ago but, at that time, it was determined that those items fielded under the old short titles could retain their CRYPTO caveat. Presently, only the "key" used to protect communication is CRYPTO - not the equipment - unless the key is installed. All new equipment will have the correct nomenclature when it is fielded.
h. Configuration item (CI): An aggregation of hardware/software or any of its discrete portions which satisfies an end use function and is designated by the government for configuration management. The CI number and the Figure A (Fig A) number mean the same thing.
i. Critical nuclear weapons design information (CNWDI): Top Secret-Restricted Data or Secret-Restricted Data revealing the theory of operation or design of the components of a thermonuclear or implosion type fission bomb, warhead, demolition munitions or test device. Information concerning arming, fusing and firing systems; limited life components; and total contained quantities of fissionable, fusionable and high explosive materials by type are excluded. Among those excluded items are components that service personnel set, maintain, operate, test or replace. See RV guides and the DOE/DOD Joint Nuclear Weapons Classification Guide and the Air Force Security Classification Guide for Nuclear Weapons.
j. Deployment module: That portion of the post-boost vehicle (PBV) which consists of the means for mounting and releasing RVs and penetration aids. It may or may not include the post-boost control system (PBCS).
k. Formerly Restricted Data (FRD): Information removed from the Restricted Data category upon determination jointly by the Department of Energy (DOE) and Department of Defense that such information relates primarily to military utilization of atomic weapons and that such information can be adequately safeguarded as classified defense information.
l. Hardness: A measure of the ability of a system to withstand exposure to one or more effects of manmade hostile environments. The resistance or degree of resistance to nuclear countermeasures or hostile environments such as neutron exposure or electromagnetic pulse (EMP) radiation. This definition encompasses those environments resulting from normal handling; powered flight and/or atmospheric reentry of the vehicle are not included.
m. Hardness critical item: Any item at any assembly level which is launch essential and/or mission critical or could adversely impact launch-essential or mission-critical equipment if hardness were not considered.
n. Latch-up time: The time required by the security subsystem to detect and hold a security violation to assure interrogation of the Launch Facility (LF) by the Missile Alert Facility (MAF).
o. Launch essential: An item of equipment or a subsystem function or characteristic is launch-essential if it is required in order to launch the missile from its silo or whose malfunction would prevent such launch in a pre-, trans- or post- nuclear attack environment.
p. Maneuvering Reentry Vehicle (MaRV): The concept of a RV as an independent entity capable of altering its own course after release from the booster. It does not cover manned vehicles.
q. Minuteman (MM) Weapon System: The MM weapon system includes the WS-133B or WS-133AM facilities, LGM30B, LGM30G missiles, MK11 Series, MK12 and MK12A RSs.
r. Missile guidance set (MGS): That portion of the missile which measures the missile position and attitude and provides control signals to all stages of the missile.
s. Mission critical (MC): An item of equipment or a subsystem function is MC if it is required to launch a missile within a given time span or to successfully complete the mission or whose malfunction would prevent such mission completion. Successful completion of the mission includes:
(1) RV delivered within acceptable CEP limits
(2) RV retains proper fuzing control
(3) System retains its
retargeting capability
(4) System retains redundancy
in communications (cable and radio)
(5) System retains valid
status reporting capability
(6) System retains specified
emergency and extended survivability capability.
t. Multiple Independent Reentry Vehicle (MIRV): The concept of one booster carrying multiple reentry vehicles which can be aimed at separate targets.
u. Peacekeeper (PK) Weapon System: The PK weapon system consists of the LGM-118 missile, WS-133 AM missile alert and launch facilities modified with a unique PK canister system for support and launch of the PK missile, and MK21 RSs.
v. Penetration aids (Pen aids): Elements such as decoys and chaff which increase the probability of successful RV penetration of an area which is defended against ballistic missile attack.
w. Post-boost vehicle (PBV): That portion of a missile which performs its primary function after separation from the prime launch vehicle and which consists of a payload (single/multiple RVs and/or Pen Aids), structure and equipment for providing guidance and control, propulsion and deployment of the payload. This includes PBCS and PSRE.
x. Propulsion system rocket engine (PSRE): That portion of the PBV which provides linear acceleration in any direction attitude control and angular acceleration about the pitch and yaw axes.
y. Reentry system (RS): Portions of the ICBM or payload which have an active role to perform after third stage thrust termination. This usually includes the RV, Pen Aids and Pen Aids wafer on the MM II and the support payload platform, Pen Aids and RVs on the MM III.
z. Reentry vehicle (RV): That part of a ballistic missile designed to reenter the earth's atmosphere in the terminal portion of the trajectory. Its prime purpose is to enable an internal payload to survive the severe environment encountered during reentry until impact or warhead detonation. In the strictest sense of the word, the term RV automatically includes the payload or warhead.
aa. Reliability: The probability that an item will perform its intended function for a specified interval under stated conditions. Normally data sets, such as those contained in maintenance failure/status reporting systems, are unclassified because they do not contain all the elements necessary to determine reliability as defined above. If any data set describes a specific vulnerability or limitation, it will be classified in accordance with the specific area of this Guide covering the system/subsystem described by that data set.
ab. Restricted Data (RD): All data concerning (1) design, manufacture or utilization of atomic weapons, (2) the production of special nuclear material or (3) the use of special nuclear material in the production of energy but shall not include data declassified or removed from the RD category pursuant to the Atomic Energy Act of 1954, Section 142.
ac. SUAVE: Silo Upgrade Addressing and Verification program.
ad. Subassembly: The first major subdivision of an assembly.
ae. Subsystem: The first major subdivision of a system, e.g., of the missile system, the propulsion subsystem.
af. TSEC: Transmission security designation used for COMSEC items.
ag. Train: As related to the weapon systems, the term "train" refers to a reentry train. A reentry train consists of a series of objects in one of three configurations (i.e., chaff alone, RV with chaff or RV alone) which are deployed from a common RS and are targeted to arrive on the same target at approximately the same time. Any of the three configurations can also have its payload deployed in any train combination. The reentry train is sometimes referred to as a cloud train due to the presence of chaff clouds after chaff deployment.
ah. Unclassified Controlled Nuclear Information: Unclassified information pertaining to the physical protection of special nuclear material in accordance with Section 1123 of Public Law 100-180. Interim procedures are contained in Under Secretary of Defense, Security Policy, Memorandum, Subject: Interim Guidance for Identifying and Controlling Unclassified Controlled Nuclear Information (UNCI) dated 18 Sep 1988.
ai. Vulnerability: The characteristics of a system which cause it to suffer a degradation (reduced capability to perform the designated mission) as a result of having been subjected to a certain level of each effect in a manmade hostile environment.
aj. VNTK: An acronym which stands for VN - vulnerability, T - type of device and K - constant. It is a term used for assessing hardness achieved at a silo, squadron, wing or the force.
ak. Weapon system: All elements necessary to attain an operational missile capability, i.e., research and development, missiles, test and training programs, launch complexes, support bases, launch and support organizations, etc.
SECTION V
DISTRIBUTION
20 AF/CC, Ste 1, /DO, Ste 2, /SE, Ste 4,/ LG, Ste 3,
7100 Saber Rd
20AF/MOC 6600 HQ Drive - 3943
Francis E Warren AFB, WY 82005-xxxx
22nd AF/SOM Travis AFB, CA 94535-5000
30 OG/CC, 747 Nebraska Ave, Ste 32, -6292 30 LG/CC, 747 Nebraska Ave, Ste 31, -6921
30SW/XPOD, 747 Nebraska Ave, Ste 34,-6294
576 FLTS/TEE, 1786 Utah St, Ste A
SMC/Det 9/ENM, 1515 Iceland Rd, Ste A
Chief, KMR Field Office/Attn: CSSD-KA-RV
P.O. Box 5309, -0930
Vandenberg AFB, CA 93437-5000
321 MG/CC OGCC
FMS
319 SPS/SPAI
MAIL ALL COPIES TO
450 G St, Ste 321
Grand Forks AFB, ND 58205-6023
341 MG/CC OG/CC
FMS
43 SPS/SPAII
MAIL ALL COPIES TO
341 MAG, BLDG 500, STE 148, 2177 St N.
Malmstrom AFB, MT 59402-7538
341 SW/LGLOJ 2177 Street North
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4220 Weapons System Evaluation Squadron Offutt AFB, NE 68113-5001
625 MOF/TAB 901 SAC BLVD
Ste 2B23
Offutt AFB, NE 68113
650 ABW/CE 225 North Rosemond Blvd
Edwards AFB, CA 93524-8540
6595 Test and Evaluation Group/MTP Vandenberg AFB, CA 93437-5000
750 SPTS/SPA, Box 051, -1236 750 SGP/OL-A-DOO, Box 061, -1237
1808 Lockheed Way
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90 MG/CC OS
LG
SSS/SPAI
MAIL ALL COPIES TO:
5305 Randall Ave
Francis E Warren AFB, WY 82005-2274
91 MG/CC OS
OMMS
FMMS
5 SPS/SPAI
MAIL ALL COPIES TO
5 MSS/MSIAC, 220 Peacekeeper PL
Minot AFB, ND 58705-5000
95 SPTG/AS 15 South Munroc Dr
Edwards AFB, CA 93524-8040
ACDA Classification Advisor US Arms Control & Disarmament Agency
320 21st Street NM
Washington DC 20451
SP - 100 Kindel Dr, Ste C301, - 5000 Arnold AFS, TN 37389-xxxx
Aerojet Propulsion Division ATTN: Crawford Butler
Bldg 2006, Dept 1711
PO Box 13222
Sacramento, CA 95813-6000
Aeromet, Inc ATTN: Facility Security Officer
PO Box 701767
Tulsa, OK 74170-1767
AFMC Wright Patterson AFB, OH 45433-5006
4375 Chidlaw Road
SP
SC
AFMC/SPO, Ste 5E21, 4255 Logistics Ave, -5760/
XRS, STE 6, 4315 Chidlaw Rd, -5006
ASC/SP, Rm 103A, 1801 10th St, -6825
1970 3rd St, -6504
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AFSAA/SAI 1580 Air Force Pentagon
Washington DC 20330-1580
AFSPC SD/SPI LAAFB/ PO Box 92969
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AFTAC/DOJ 1030 South Highway AIA
Patrick AFB, FL 32925-3002
Attn: Capt. McCobb
Air Force Media Center AFMEC/SP
1363 Z St, Bldg 2730
March AFB, CA 92518-2717
Alliant Techsystems, Inc Bacchus Works (ATTN: Security Supervisor)
PO Box 98
Magna, UT 84044
Allied Signal Aerospace Electronics Systems
ATTN: Security Department
250 Knotter Drive
Cheshire, CT 06410
Appraisal and Disposition Section Records Group 342
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Atlantic Research Corp 5945 Wellington Road
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Atlantic Research Corporation Liquid Propulsion
PO Box 300 LPO
6686 Walmore Rd
Niagara Falls, NY 14304-0300
Atlantic Research Corporation Liquid Propulsion
PO Box 771
Clearfield, UT 84015
AVCO Corporation Textron Defense Systems Division
ATTN: Security Supervisor
201 Lowell Street
Wilmington, MA 01887
AWFL/SP Kirtland AFB, NM 87115-5000
Batelle Columbus Laboratories ATTN: Security Officer
505 King Avenue
Columbus, OH 43201-2693
Boeing Guidance Repair Center Attn: Security
813 Irving-Wick D West
Newark AFS, OH 43055-5149
Boeing North American Autonetics Strategic Systems Division
3370 Miraloma Ave
Anaheim, CA 92803
Boeing North American Autonetics Strategic Systems Division
ATTN: K. George
6039 Wardleigh Rd
Hill AFB, UT 84056-5838
Capitol Hill Area, DIS Hoffman Building
2416 Eisenhower Avenue
Alexandria, VA 22331-1000
Central Region, DIS Mid-Western Region
610 South Canel Street, Room 908
Chicago, IL 60607-4599
Central Region, DIS Southwestern Sector
106 Decker Court, Suite 200
Irving, TX 75062-2795
Charles Stark Draper Laboratories, Inc ATTN: Document Control
Mail Station 74
555 Technology Square
Cambridge, MA 02139
Chief National Archives Federal Archives & Records Center, NARA
24000 Avila Road
Laguna Niguel, CA 92656-3497
Commander US Army Missile Command
AMSMI-WS-SA
ATTN: Mr Seinford
Redstone Arsenal, AL 35898
Commander, Field Command
Defense Nuclear Agency
ATTN: FCSS
1680 Texas St SE
Kirtland AFB, NM 87117-5669
Commander, USAKA ATTN: CSSD-KA-RO
P.O. Box 26
APO San Francisco, CA 96555
Commanding Officer Naval Explosive Ordnance Disposal Center
ATTN: Tech Library Division
Indianhead Naval Station, MD 20640-5000
DCASMA BOSTON ATTN: FACC-C2
495 Summer St
Boston, MA 01120-2109
DCG USASSDC ATTN: CSSD-TE-O/CSSD-KA-RH
P.O. Box 1500
Huntsville, AL 35807-3801
Defense Nuclear Agency/ISCM Washington DC 20305-2000
Defense Technical Information Center Building 5, Cameron Station
Alexandria, VA 22304-6145
Deputy Director Security Classification Safeguards DISS, ODASD(CISCM), OASD (C31)
The Pentagon, Rm 3C274
Washington DC 20301-3040
DET 1 OO-ALC 901 SAC Blvd, Ste 1F21
Offutt AFB, NE 68113-5660
Director National Imagery Mapping Agency Aerospace Center
ATTN: SO (Jack Cumbow)
3200 South Second St
St Louis AFB, MO 63118-3399
Director National Imagery Mapping Agency
ATTN: ISA ST A-15 (H. Ketts)
Fairfax, VA 22031-2137
Director of Security Plans and Programs Office of the Deputy Under Secretary of Defense (Policy)
Washington CD 20301-2000
Director or Information Security Ofc of the Dep Under Sec of Defense (Policy)
Washington DC 20301-0001
Directorate, Freedom of Information and Security Review Office of the Assistant Secretary of Defense
(Public Affairs)
1400 Defense Pentagon
Washington DC 20301-1400
DISA/DO 701 S. Court House Rd
Alexandria, VA 22204-2219
DMA Bldg 56, ATTN: PR
US Naval Observatory
Washington DC 20350
DMAAC/GCB ATTN: Operations Division
P.O. Box 9617
Francis E Warren AFB, WY 82005-6300
DPMC The Boeing Company
PO Box 3707
Seattle, WA 98124-2207
DPMC Rockwell International
Rocketdyne Division
6633 Canoga Avenue
Canoga Park, CA 91303-2790
DPMC Northrop Corporation
2301 W. 120th Street
Hawthorne, CA 90250-3363
DPMC Martin Marietta Aerospace
Denver Division
PO Box 179
Denver, CO 80201-1079
DPMC Morton Thiokol Corporation
Wasatch Division
PO Box 524, MS-250
Brigham City, UT 84032-0524
DPMC GTE Government Systems Corporation
360 First Avenue
Needham Hts, MA 02194-2787
DPMC Hercules Inc
Aerospace Division
PO Box 98
Magna, UT 84044-0098
DPMC Aerojet General Corporation PO Box 15846
PO Box 15846
Sacramento, CA 95852-1846
DPMC General Electric Astrospace Division
ATTN: Security
23 Goddard Blvd
King of Prussia, PA 19406-2902
DPMC DET 40 AVCO Corporation
Textron Defense Systems
201 Lowell Street
Wilmington, MN 01887-2941
DPMC Rockwell International Corp 3370 Mira Loma
Anaheim, CA 92803-3110
DPMC San Antonio Austin Residency
6500 Tracor Lane
Austin, TX 78725-2000
DPMC TRW 1 Space Park, E1/1081
Redondo Beach, CA 90278-1078
DTIC Cameron Station
Alexandria, VA 22304-6100
Dynamics Research Corporation ATTN: Security Office
60 Concord St
Wilmington, MA 01887-2934
Ertec Western, Inc ATTN: Security Office
3777 Long Beach Blvd
Long Beach, CA 90807-3309
General Electric Company Ordnance Systems Division
100 Plastic Ave
Pittsfield, MA 01201-3698
Gilbert Associates, Inc ATTN: Security Office
PO Box 1498
Reading, PA 19603-1498
GTE Government Systems Corporation 3502 Lincoln Ave, Ste 4
Ogden, UT 84401
GTE Government Systems Corporation ATTN: Security Supervisor
77 ìAî Street
Needham, MA 02194
Hercules Inc Aerospace Division
Bacchus Works
ATTN: Security Office
PO Box 98
Magna, UT 84044-0098
Honeywell, Inc ATTN: Dee Burch, M/S 190-1
13350 US Highway 19N
Clearwater, LF 34624-7290
HQ AETC/ AOS/AOX, Ste 2, 1 F ST, -4325
Randolph AFB, TX 78148-xxxx
HQ AFHRA/ISR 600 Chennault Circle
Maxwell AFB, AL 36112-6424
HQ AFHSO/HOS 170 Luke Ave Suite 400
Bolling AFB, DC 20332-5113
HQ AFIA/IM 6700 G Ave SE
Kirtland AFB, NM 87117-5670
HQ AFOTEC/SP, 85OO Gibson Blue, SE, -5558
377 SPS/CC/SPA, 1351 1st St SE, -5527
OL-NS/ENG, 1651 1st St SE, -5617
AFMC NSO/SWN, 1680 Texas St SE, -5669
Kirtland AFB, NM 87117-xxxx
HQ AFSC/SEW 9700 Avenue G SE
Kirtland AFB, NM 87117-5670
HQ AFSPC CEF/CC 1520 E Willamette Ave
Colorado Springs, CO 80909-4554
HQ AFSPC/ DLM -4180
DOT -4240
DOM -4180
DOMN -4180
DRM -4760
LGM -4470
SCMB -4400
SEWM -4260
SFPON -4560
150 Vandenberg St, Ste 1105
Peterson AFB, CO 80914-xxxx
HQ DIS Industrial Security Office (VO410) 1340 Braddock Pl
Alexandria, VA 22314-1651
HQ DNA/ISIS 6801 Telegraph Rd
Alexandria, VA 22310-3390
HQ RL/SP 26 Electronic Parkway
Griffiss AFB, NY 13441-4514
HQ USAF XOFS/XOOB/XORS/XORW
1480 Air Force Pentagon, -1480
LGSW/LGMW
1030 Air Force Pentagon, -1030
SEC
1400 Air Force Pentagon, -1400
Washington DC 20330-xxxx
HQ USAF/SPI 1340 Air Force Pentagon
Washington DC 20330-1340
HQ USSTRATCOM/ J-005, Ste 1H9, -6005
J-312/-331-334-362/-441/-443,
Ste BA3, -8300
J-511/-541, Ste 2E8, -6500
J-523, Ste 2E8, -6500
J-611, Ste 2B9, -6600
901 SAC Blvd
Offutt AFB, NE 68113-xxxx
ITT Federal Services Corporation ATTN: Facility Security Officer
PO Box 5728
Vandenberg AFB, CA 93437
Johnson Controls World Services, Inc ATTN: Document Control
401 Wynn Drive
Huntsville, AL 35805
Johnson Controls World Services, Inc ATTN: Document Control
PO Box 1761
APO San Francisco, CA 96555
KMR Weather Station Aeromet, Inc
PO Box 67
APO San Francisco, CA 96555
Lawrence Livermore Laboratory ATTN: Classification Office (L-302)
PO Box 808
Livermore, CA 94551-9900
Litton Systems Inc G&C Systems Division
5500 Canoga Avenue
Woodland Hills, CA 91365-6698
Lockheed-Martin ATTN: Facility Security Officer, M/S 13B
9970 Federal Drive
Colorado Springs, CO 80921-3697
Lockheed-Martin Missiles and Space Valley Forge Operation
ATTN: Security Supervisor
230 Mall Blvd
King of Prussia, PA 19406-2995
Lockheed-Martin Missiles and Space ATTN: Security Supervisor
PO Box 3504
Sunnyvale, CA 94088-3504
Logicon, Inc ATTN: Security Supervisor
PO Box 471
San Pedro, CA 90733-0471
Logicon, Inc ATTN: Security Supervisor
3701 Skypark Dr, Ste 200
Torrance, CA 90505-4794
Los Alamos National Laboratory ATTN: Group OS6
PO Box 1663
Los Alamos, NM 87545
MAC/SP Scott AFB, IL 62225-5001
Maxwell Labs, Inc S-Cubed Division
ATTN: Security
PO Box 1620
LaJolla, CA 92038-1620
McDonnell Douglas ATTN: Denise Schmate
5201 Bolsa Avenue
Huntington Beach, CA 92647-0299
MIT Lincoln Laboratory ATTN: KREMS Site Manager
PO Box 58
APO San Francisco, CA 96555-5000
MIT/Lincoln Laboratory/KREMS ATTN: Bing Potts
PO Box 58
APO San Francisco, CA 96555
MIT/Lincoln Laboratory/KREMS Data Library ATTN: Document Control
PO Box 73
244 Wood Street
Lexington, MA 02173-9108
Morton Thiokol, Inc Wasttch Division
ATTN: Security Office
PO Box 524
Brigham City, UT 84032-0524
National Archives and Records Admin (NIR) Records Group 342
Washington, DC 20408-0001
National Security Agency Attn: DDI
9800 Savage Rd
Fort George Meade, MD 20755-6000
Northeast Region, DIS Mid-Atlantic Sector
1040 Kings Highway North
Cherry Hill, NJ 08034-1908
Northeast Region, DIS New England Sector
495 Summer Street
Boston, MA 02210-2192
Northrop Corporation Electronics Division
ATTN: Security Office
2310 W. 120th Street
Hawthorne, CA 90251-5032
NSA-Asst Dir NSA for COMSEC Ft George G. Meade, MD 20755-5000
NSA/DDI 9800 Savage Rd
Fort George Mead, MD 20755-6700
OL-AA, Phillips Laboratory/XPG Attn: Noreen Diamond
29 Randolph Rd
Hanscom AFB, MA 01731-3010
OL-AC, Phillips Laboratory/SP ATTN: Danny Green
5 Pollux Dr
Edwards AFB, CA 93524-7062
ONRR Massachusetts Institute of Technology
Lincoln Laboratory/RM E19-628
77 Massachusetts Avenue
Cambridge, MA 02139-4307
OO-ALC/ PA, 7981 Georgia St, -5824
TI/TIE, 5851 F St, -5713
75 SFS/SFAI 6010 Gum LN, -5825
649 EOD/ESO, 6316 Juniper Dr, -5931
Hill AFB UT 84056-xxxx
Orbital Sciences Corporation Space Data Division
ATTN: Security Supervisor
3380 South Price Rd
Chandler, AZ 85248
Pacific Region, DIS Southern and Northern Sector
3605 Long Beach Blvd, Suite 405
Long Beach, CA 90807-4013
Palisades Geophysical Institute, Inc PO Box 1751
Cape Canaveral, FL 32920-1751
Pan Am World Services, Inc ATTN: Range Operations Manager
PO Box 1761
APO San Francisco, CA 96555-5000
R. A. Hanson Company, Inc ATTN: Security Office
PO Box 7400
Spokane, WA 99207-0400
Raytheon Company ATTN: Security Supervisor
528 Boston Post Road
Sudbury, MA 01776
Rockwell International Corporation Rocketdyne Division
ATTN: Security Office
6633 Canoga Avenue
Canoga Park, CA 91303-2790
Rockwell International Corporation Rocketdyne Division
ATTN: Security
PO Box 59098
Vandenberg AFB, CA 93437-5000
SA-ALC NW, 413 Jackson, -5314
76SPS/SPA, 206 Duncan Dr, -5936
Kelly AFB, TX 78241-xxxx
SA-ALC/NWIS 1651 First Street SE
Kirtland AFB, NM 87117-5617
SAF/AAZD c/o HQ AU
55 LeMay Plaza South
Maxwell AFB, AL 36112-6335
Sandia National Laboratories ATTN: R.E. Martinell, 8535
Classification Officer
PO Box 969
Livermore, CA 94551-0969
Science Applications International Corporation ATTN: Security Supervisor
10260 Campus Point Dr
San Diego, CA 92121-1578
SDIO/DSIM The Pentagon, Rm 1E1062
Washington DC 20330-7100
Secretary of the Air Force AQQS(M),
1060 Air Force Pentagon, -1060
PAS
1690 Air Force Pentagon, -1690
Washington DC 20330-xxxx
Southeastern Region, DIS 2300 Lake Park Drive, Suite 250
Smyrna, GA 30080-7606
The Aerospace Corporation ATTN: Classification Management
PO Box 92957
Los Angeles, CA 90009
The Boeing Company ATTN: Security Supervisor
PO Box 3707
Seattle, WA 98124
The Boeing Company ATTN: Security
PO Box 1004
Clearfield, UT 84015
Thiokol Wasatch Division
PO Box 524
Brigham City, UT 84302
TRW Data Technologies Division ATTN: Security
PO Box 6213
Carson, CA 90749
TRW Space and Electronics ATTN: Security Supervisor
One Space Park
Redondo Beach, CA 90278
TRW Strategic Systems Division ATTN: Security
PO Box 1310
San Bernardino, CA 92402
TRW Strategic Systems Division Systems Integration Group
1104 Country Hills Drive
Ogden, UT 84403-2400
United Technology Corporation Chemical Systems Division
ATTN: Document Control
PO Box 49028
San Jose, CA 95161-9028
US DOE/Classification Division P O Box 5400
Albuquerque, NM 87185-5400
Weidlinger Associates ATTN: Dr. Jeremy Isenberg
620 Hanson Way, Suite 100
Palo Alto, CA 94303-1014
Westinghouse Electric Corporation Marine Division
ATTN: Debra Martin
PO Box 3499
Sunnyvale, CA 90488-3499
XONTECH, Inc ATTN: Security Supervisor
6151 West Century Blvd
Los Angeles, CA 90045
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FUNDING, PROCUREMENT AND PRODUCTION
Information RevealingClassification
Reason
Date
Remarks
1 Complete funding for the entire WS-133A, WS-133B or WS-133AM program (including all appropriations) for the current and subsequent fiscal years except RV funds. S-FRD
1.5.a (X2)
UNCLASSIFIED after DOD release. See RV guides for RV funding data classification. 2 Complete funding to date, including the current fiscal year for the entire WS-133B and WS-133AM programs. U
Includes numbers delivered and rate of delivery. 3 Complete funding for any one R&D or production contract.
a. Total unit cost of any missile. U
b. Total unit cost of any subsystem. U
For warheads, see RV guides. 4 Parts, accessories and equipment available on the open market. U
5 Provisioning parts breakdown except RV. U
See RV guides. 6 Production data on operational force missile.
a. Total number of missiles to be produced on a given contract. U
b. Total number of missiles produced on all contracts. U
c. Total number of missiles planned for future production. U
d. Total number of missiles that have been have delivered to an operational site. U
7 Production data on R&D missiles:
a. Total number of missiles planned or programmed. U
b. Total number of missiles that are produced on a given contract. U
8 Subsystem production:
a. Total number of subsystems for future production for operational use except RV. U
For RVs, see applicable RV guides. b. Total number of subsystems planned for future production for R&D use. U
c. Total number of subsystems that have been produced on all contracts. U
d. Total number of subsystems that have been produced on all contracts. U
e. Warhead subsystems production information. U
See applicable RV guides. f. Pen Aids subsystems production quantities. U
See Section XVII and XVIII.
HARDWARE CLASSIFICATION
See USSTRATCOM SD 501-12 for items identified as requiring special
handling.
Information Revealing |
Visual Access |
Physical Access |
Remarks |
|
1 | Propulsion subsystem: | |||
a. Complete Stage 1 propulsion subsystem, including nozzles | U |
U or S 1.5.g (X2) |
Stage 1 subsystem is UNCLASSIFIED prior to installation of classified P-89, Stage 1 nozzle control units. SECRET for those subsystems with classified P-89s installed. | |
b. Complete Stage 2 propulsion subsystem, including nozzles for MM I (WS-133A) | U |
U |
||
c. Complete Stage 2 of MM II and III. | U |
U or S DECLAS 31 Dec 2007 |
Stage 2 subsystems UNCLASSIFIED prior to installation of classified P-90, Stage 2 attitude control group. SECRET for subsystems with classified P-90s installed. | |
d. Complete Stage 3 of MM III propulsion subsystem, including nozzle. | U |
U or S DECLAS 31 Dec 2007 |
Stage 3, MM III subsystems, UNCLASSIFIED prior to installation of classified P-116, liquid injection thrust vector control (LITVC) unit. SECRET for subsystems with classified P-116s installed. | |
e. Complete Stage 3 of MM II propulsion subsystem, including engine nozzles and thrust termination component. | U |
U or S DECLAS 31 Dec 2007 |
Stage 3, MM II subsystems UNCLASSIFIED prior to installation of classified P-91, Stage 3 nozzle control units. SECRET for subsystems with classified P-91s installed. | |
f. Complete PSRE | U |
U |
||
g. Angular accelerometer between Stage 2 and 3, P-68. | U |
U or S DECLAS 31 Dec 2007 |
Unit UNCLASSIFIED prior to P/N 25170-102-21. SECRET for P/N-21s. | |
h. Nozzle control unit Stage 1, P-89 | U |
U or S DECLAS 31 Dec 2007 |
UNCLASSIFIED prior to P/N 25340-102-581. SECRET for P/N-581s and higher. | |
i. Attitude control group, Stage 2, P-90 | U |
U or S DECLAS 31 Dec 2007 |
UNCLASSIFIED prior to P/N 25333-102-551. SECRET for P/N 551s and higher. | |
j. Nozzle control unit, Stage 3, P-91 | U |
U or S DECLAS 31 Dec 2007 |
UNCLASSIFIED prior to P/N 25341-102-581. SECRET for P/N 581s and higher. | |
k Cable assembly, Stage 1, P-93 | U |
U |
||
l. Cable assembly, Stage 2, P-113 | U |
U |
||
m. Cable assembly, Stage 3, P-114 | U |
U |
||
n. LITVC unit, P-116. | U |
S DECLAS 31 Dec 2007 |
Classification due to presence of hardness material | |
o. Complete ordnance cable assembly for Stage 2, MM II retrofit, and Stage 2, MM III, Block IV, and Stage 3, MM II & III, Block IV. | U |
U |
||
p. Complete aluminum ground strip assembly for MM III, Stage 3, Block IV. | U |
U |
||
q. Complete roll control valve junction box and cable assembly for MM II, Stage 2 retrofit, and MM III, Stage 2, Block IV. | U |
U |
||
r. Complete raceway conductive strip assembly for Stage 3, MM III, Block IV. | U |
U |
||
s. Complete boosters: | ||||
|
U |
U or S DECLAS 31 Dec 2007 |
Physical access will be classified SECRET if any classified components described in 1.a. through 1.j. above are incorporated. | |
|
U |
S DECLAS 31 Dec 2007 |
Classified SECRET unless all classified hardware is removed. All operationally configured boosters are SECRET. | |
|
U |
S DECLAS 31 Dec 2007 |
See Remark in 1.s.(2) above | |
2 | Reverse thrust subsystem: | |||
a. Reverse thrust subsystem | U |
U |
||
b. Complete roll control and LITVC system in Stage 2, Wing VI, and subsequent. | U |
U |
||
c. Retro-rocket motor | U |
U |
||
d. Tumble rocket motor | U |
U |
||
|
e. A portion of cured propellant for rocket motors. | U |
U |
|
3 | Guidance subsystem: | |||
a. MGS (NS10) which includes the stabilized platform, computer, magnetic memory. | U |
C DECLAS 31 Dec 2007 |
This subsystem is no longer deployed in the weapon system. It is used at Vandenberg AFB. Classified due to presence of design information currently used in NS17 units. | |
b. MGS (NS17): | U |
TS-CRYPTO DECLAS 31 Dec 2007 |
Physical access to this subassembly is SECRET to TOP SECRET CRYPTO. The computer can be SECRET to TOP SECRET-CRYPTO and requires special handling as outlined in USSTRATCOM SD 501-12 when the memory contains MM codes/SIOP data. | |
|
U |
S DECLAS 31 Dec 2007 |
P/Ns 9214-300001-571 and -581. Physical access to the body section and many other radiation shielding parts is classified SECRET because the material could be identified and radiation shielding capability determined. | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 67369-301. See 3.b.(1) | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 69207-201. See 3.b.(1) | |
|
U |
C DECLAS 31 Dec 2007 |
P/N 67439-301. Physical access to the inertial instruments is classified CONFIDENTIAL because testing could determine the accuracy capability of the instrument. Inertial instruments are unclassified when not in operational condition. | |
|
U |
C DECLAS 31 Dec 2007 |
P/N 66777-302. Physical access to inertial instruments is classified CONFIDENTIAL because testing could determine the accuracy capabilities of the instrument. | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 65541-402. See 3.b.(1) | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 68076-201. See 3.b.(1) | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 68081-201. See 3.b.(1) | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 69737-201. See 3.b.(1) | |
|
U |
C DECLAS 31 Dec 2007 |
P/N 102500. Physical access to the inertial instruments is classified CONFIDENTIAL because testing could determine the accuracy capability of the instrument. Inertial instruments are unclassified when not in operational condition. | |
|
U |
TS-CRYPTO DECLAS 31 Dec 2007 |
P/N 55032-106. Classification is dependent upon information contained in the memory. Special handling required as outlined in USSTRATCOM SD 501-12 , Vol I when unit contains MM codes/SIOP data. | |
|
U |
TS-CRYPTO DECLAS 31 Dec 2007 |
P/N 64128-501. Classification is dependent upon information contained in the memory. Special handling required as described in 3.b.(11). | |
|
U |
TS-CRYPTO DECLAS 31 Dec 2007 |
P/N 55713-304. Classification is dependent upon information contained in the memory. Special handling required as described in 3.b.(11) | |
|
U |
S DECLAS 31 Dec 2007 |
P/Ns 8541-303378 and 8541-303380. See 3.b.(1) | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 69437-201. See 3.b.(1). | |
|
U |
C DECLAS 31 Dec 2007 |
P/N 78170. Physical access to the inertial instruments is classified CONFIDENTIAL because testing could determine the accuracy capability of the instrument. Inertial instruments are unclassified when not in operational condition. | |
c. MGS (NS20): | U |
S to TS-CRYPTO DECLAS
31 Dec 2007 |
Physical access to this subassembly is SECRET to TOP SECRET-CRYPTO depending on what information is in the computer memory. The computer/NS-20 requires special handling outlined in USSTRATCOM SD 501-12 when it contains MM codes/SIOP data. | |
|
U |
C DECLAS 31 Dec 2007 |
P/N 67776-301. Physical access to the inertial instruments is classified CONFIDENTIAL because testing could determine the accuracy capability of the instrument. Inertial instruments are unclassified when not in operational condition. | |
|
U |
C DECLAS 31 Dec 2007 |
P/N 66777-302. Physical access to the inertial instruments is classified CONFIDENTIAL because testing could determine the accuracy capability of the instrument. Inertial instruments are unclassified when not in operational condition. | |
|
U |
C DECLAS 31 Dec 2007 |
P/Ns 68110-301 and 968110-301. See 3.c.(4) below | |
|
U |
S DECLAS 31 Dec 2007 |
P/Ns 70752-201 and 68160-301. Physical access to radiation shielding parts is classified SECRET because material could be identified and radiation shielding capability determined. | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 70754-201. See 3.c.(4). | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 70768-201. See 3.c.(4). | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 70771-201. See 3.c.(4). | |
|
U |
C DECLAS 31 Dec 2007 |
P/N 78170. Physical access to the inertial instruments is classified CONFIDENTIAL because testing could determine the accuracy capability of the instrument. Inertial instruments are unclassified when not in operational condition. | |
|
U |
C DECLAS 31 Dec 2007 |
P/N 102500. Physical access to the inertial instruments is classified CONFIDENTIAL because testing could determine the accuracy capability of the instrument. Inertial instruments are unclassified when not in operational condition. | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 70602-201. See 3.c.(4). | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 70603-201. See 3.c.(4). | |
|
U |
S to TS-CRYPTO DECLAS
31 Dec 2007 |
P/N 55035-106. Classification is dependent upon information contained in the memory. Special handling required as directed by USSTRATCOM SD 501-12 Vol I, when unit contains MM codes/SIOP data. | |
|
U |
S to TS-CRYPTO DECLAS
31 Dec 2007 |
P/N 31200-501. Classification is dependent upon information contained in the memory. Special handling required as noted in 3.c.(12). | |
|
U |
S to TS-CRYPTO DECLAS 31 Dec 2007 |
P/N 56213-304. Classification is dependent upon information contained in the memory. Special handling required as noted in 3.c.(12). | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 70601-201. See 3.c.(4) | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 70800-201. See 3.c.(4). | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 25343-102. See 3.c.(4). | |
|
U |
S DECLAS 31 Dec 2007 |
P/Ns 70589-201 and 56973-501. See 3.c.(4). | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 57940-507. See 3.c.(4). | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 70814-507. See 3.c.(4). | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 70815-507. See 3.c.(4). | |
|
U |
U |
P/N 8537-404223. | |
d. MGS (NS50): | U |
S 1.5.g (X2) |
Physical access to this subassembly is either SECRET to TOP SECRET-CRYPTO depending on what information is in the computer memory. The MGS requires special handling outlined in ACCR 55-56 when the computer (MGC) contains MM codes/SIOP data. | |
|
U |
S 1.5.g (X2) |
P/Ns 13400-301 and 968110-301. See 3.c.(4). | |
|
U |
C 1.5.g (X2) |
P/N34108700. Physical access to the inertial instruments in classified CONFIDENTIAL because testing could determine the accuracy capability of the instrument. Instruments are unclassified when not in operational condition. | |
|
U |
C 1.5.g (X2) |
P/N 66777-302. Physical access to the inertial instruments is classified CONFIDENTIAL because testing could determine the accuracy capability of the instrument. Instruments are unclassified when not in operational condition. | |
|
U |
S 1.5.g (X2) |
P/Ns 70752-201 and 68160-301. Physical access to radiation shielding parts is classified SECRET because material could be identified and radiation shielding capability determined. | |
|
U |
S 1.5.g (X2) |
P/N 70754-201. See 3.c.(4). | |
|
U |
S 1.5.g (X2) |
P/N 70768-201. See 3.c.(4). | |
|
U |
S 1.5.g (X2) |
P/N 70771-201. See 3.c.(4). | |
|
U |
C 1.5.g (X2) |
P/N 78170. Physical access to the inertial instruments is classified CONFIDENTIAL because testing could determine the accuracy capability of the instrument. Instruments are unclassified when not in operational condition. | |
|
U |
C 1.5.g (X2) |
P/N 102500. Physical access to the inertial instruments is classified CONFIDENTIAL because testing could determine the accuracy capability of the instrument. Instruments are unclassified when not in operational condition. | |
|
U |
S 15.g (X2) |
P/N BG9761B. The MGC is classified because of the shield within the MGC. (P/N 11777-403, 11778-403 & 11779-403) and memory contents. The memory becomes unclassified when all power (flight battery and SRAM battery) is removed. See 3.c.(4). | |
|
U |
U |
P/N 8537-404223. | |
|
U |
S 1.5.g (X2) |
Physical access to radiation shielding parts is classified SECRET because material could be identified and radiation shielding capability determined. | |
|
U |
S 1.5.g (X2) |
See 3.e.(12) | |
|
U |
S 1.5.g (X2) |
See 3.e.(12) | |
|
U |
S 1.5.g (X2) |
See 3.e.(12) | |
|
U |
S 1.5.g (X2) |
See 3.e.(12) | |
|
U |
S 1.5.g (X2) |
See 3.e.(12) | |
|
U |
S 1.5.g (X2) |
See 3.e.(12) | |
|
U |
S 1.5.g (X2) |
See 3.e.(12) | |
|
U |
S 1.5.g (X2) |
See 3.e.(12) | |
|
U |
S 1.5.g (X2) |
See 3.e.(12) | |
|
U |
S 1.5.g (X2) |
See 3.e.(12) | |
|
U |
S 1.5.g (X2) |
See 3.e.(12) | |
|
U |
S 1.5.g (X2) |
See 3.e.(12) | |
|
U |
S 1.5.g (X2) |
See 3.e.(12) | |
|
U |
S 1.5.g (X2) |
See 3.e.(12) | |
|
U |
S 1.5.g (X2) |
See 3.e.(12) | |
|
U |
S 1.5.g (X2) |
See 3.e.(12) | |
|
U |
S 1.5.g (X2) |
See 3.e.(12) | |
|
U |
S 1.5.g (X2) |
See 3.e.(12) | |
|
U |
S 1.5.g (X2) |
See 3.e.(12) | |
|
U |
S 1.5.g (X2) |
See 3.e.(12) | |
|
U |
S 1.5.g (X2) |
See 3.e.(12) | |
|
U |
S 1.5.g (X2) |
See 3.e.(12) | |
|
U |
S 1.5.g (X2) |
See 3.e.(12) | |
|
U |
S 1.5.g (X2) |
See 3.e.(12) | |
|
U |
S 1.5.g (X2) |
See 3.e.(12) | |
|
U |
S 1.5.g (X2) |
See 3.e.(12) | |
|
U |
S 1.5.g (X2) |
See 3.e.(12) | |
e. Classified Economic Order Quantity (EOQ) items for NS10 and/or NS17 and/or NS20 and/or NS50: | ||||
|
U |
S DECLAS 31 Dec 2007 |
P/Ns 57780-507 and 57778-507. Physical access is classified SECRET because the shielding material could be identified and radiation shielding capability determined. | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 58200-507. See 3.d.(1). | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 54722-507 See 3.d.(1). | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 56188-507. See 3.d.(1). | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 57970-507. See 3.d.(1). | |
|
U |
S DECLAS 31 Dec 2007 |
P/Ns 57776-507 and 57339-507. See 3.d.(1). | |
|
U |
S DECLAS 31 Dec 2007 |
P/Ns 70615-201 and 70605-201. See 3.d.(1). | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 69954-201. See 3.d.(1). | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 57992-507. See 3.d.(1). | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 60801-201. See 3.d.(1). | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 57992-507. See 3.d.(1). | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 50589-507. See 3.d.(1). | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 8541-3003336. See 3.d.(1). | |
|
U |
S DECLAS 31 Dec 2007 |
P/Ns 57993-507 and 50583-507. See 3.d.(1). | |
|
U |
S DECLAS 31 Dec 2007 |
P/Ns 50575-507 and 50574-507. See 3.d.(1). | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 69737-201. See 3.d.(1). | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 60878-201. See 3.d.(1) | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 57972-507. See 3.d.(1). | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 50582-507. See 3.d.(1) | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 57973-507. See 3.d.(1). | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 67A53001P44. See 3.d.(1). | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 57790-507. See 3.d.(1). | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 483-0224-002. See 3.d.(1) | |
|
U |
S DECLAS 31 Dec 2007 |
P/Ns 50573-507 and 50577-507. See 3.d.(1). | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 56191-507. See 3.d.(1). | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 57991-507. See 3.d.(1). | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 85075-201. See 3.d.(1) | |
|
U |
S DECLAS 31 Dec 2007 |
P/Ns 57996-507 and 57782-507. See 3.d.(1). | |
|
U |
S DECLAS 31 Dec 2007 |
P/Ns 57999-507-1 and 57995-507-1. See 3.d.(1). | |
|
U |
S DECLAS 31 Dec 2007 |
P/N 69457-201-3. See 3.d.(1). | |
4 | RS Subsystem. | See Section V. | ||
5 | Warhead subsystems (RV). | See appropriate RV guide | ||
6 | Command Data Buffer: | |||
a. LCF Processor (LCFP), Fig A 14058 (applies to all drawers associated with LCFP) | U |
U or TS-CRYPTO (SIOP-ESI) 1.5.c (X1) |
LCFP rack UNCLASSIFIED with no drawers installed. TOP SECRET - CRYPTO with TSEC/KI-22 SDU Fig A 1506 and keying variable. | |
b. Programmer group (LF) Fig A 1201 (applies to all associated drawers). | U |
U or S or TS-CRYPTO 1.5.c (X1) |
Rack UNCLASSIFIED with no drawers installed. SECRET with SDU and test keying variable installed. TOP-SECRET-CRYPTO with operational keying variable installed. | |
c. Digital data terminal (LF) Fig A 14152 (and all associated drawers). | U |
U or S or TS-CRYPTO 1.5.c (X1) |
Initially UNCLASSIFIED. Special handling required. SECRET - CONTROLLED COMSEC ITEM with SDU and test keying variable installed. TOP SECRET-CRYPTO with SDU and operational keying variable installed. | |
d. IPD processor drawer CI 17791. | U |
U or S-CRYPTO or TS-CRYPTO 1.5.c (X1) |
UNCLASSIFIED when SDU and keying variables are removed. SECRET - CRYPTO with SDU and operational keying variable installed. Up to TOP SECRET-CRYPTO with contractor test IPD processor keying variable assembly installed. All other drawers and units associated are classified and handled the same. | |
e. Secure Data Unit (SDU) Fig A 1506. Transmission Security (TSEC)/KI-22T. | S 1.5.c (X1) |
SECRET Controlled COMSEC Item with no keying variable. Classification and protection determined by keying variable when installed. DECLAS According to applicable COMSEC documents/guidance for keying variable involved. | ||
f. SDU Fig A 1506, TSEC/KI-22M | U |
S 1.5.c (X1) |
SECRET Controlled COMSEC Item with no keying variable. Classification and protection determined by keying variable when installed. DECLAS According to applicable COMSEC documents/guidance for keying variable involved. | |
g. SDU Fig A 1506. TSEC/KI-22 | U |
S 1.5.c (X1) |
SECRET Controlled COMSEC Item with no keying variable. Classification and protection determined by keying variable when installed. DECLAS According to applicable COMSEC documents/guidance for keying variable involved. | |
h. Keying variables: | All keying variables are accountable as separate items when not installed and accountable under the item in which installed. | |||
|
U |
TS-CRYPTO 1.5.c (X1) |
Used with MGS in MM II, III
Information is classified because it could reveal a cryptologic system or activity (XI). |
|
|
U |
TS-CRYPTO -11, -78 -12 WG IV 1.5.c (X1) |
Used with SDU, KI-22, Fig A 1506. | |
|
U |
S-CRYPTO 1.5.c (X1) |
Used with SDU, KI-22M, Fig A 1506 in IPD modem. | |
|
U |
U or TS-CRYPTO 1.5.c (X1) |
Initially UNCLASSIFIED. Special handling required. Used with SDU, KI-22M, Fig A 1506 in IPD processor. | |
|
U |
U 1.5.g (X2) |
Controlled COMSEC Item. Used with MGS in MM II, III. | |
|
U |
S 1.5.g (X2) |
Controlled COMSEC Item. SDU Keying Variable PROM. DECLAS according to applicable COMSEC documents/guidance. | |
7 | Command control auxiliary subsystem: | |||
a. Decoder - command signals ground (CSD-G), Fig A 1268. | U |
U |
||
b. Decoder - command signals - missile (CSD-M) , Fig A 6752 | U |
U to S-CRYPTO 1.5.c (X1) & 1.5.g (X2) |
Initially UNCLASSIFIED. Special handling required. | |
c. Panel assembly launch control (Part of Console) Fig A 1243, 1243M | U |
U to S-CRYPTO 1.5.c (X1) |
Initially UNCLASSIFIED. Special handling required. | |
|
U |
U to TS-CRYPTO 1.5.c (X1) |
Initially UNCLASSIFIED. Special handling required. | |
d. Secure code unit assembly Mechanical Code Unit (MCU) | U |
U to TS-CRYPTO 1.5.c (X1) & 1.5.g (X2) |
Initially UNCLASSIFIED. Special handling required. | |
e. Wing code processing system,
(WCPS) CI 42156: |
U |
S to TS-CRYPTO 1.5.c (X1) & 1.5.g (X2) |
Initially SECRET. Special handling required. | |
|
U |
S-CRYPTO to TS (SIOP-ESI) 1.5.c (X1) |
Special handling required. | |
|
U |
TS-CRYPTO (SIOP-ESI) 1.5.c (X1) |
Until successful overwrite is accomplished. | |
|
U |
U to TS 1.5.g (X2) |
Initially UNCLASSIFIED. Special handling required. | |
f. Code change verifier CI 05201. | U |
U to TS-CRYPTO 1.5.c (X1) & 1.5.g (X2) |
Initially UNCLASSIFIED. Special handling required. | |
g. Launch Enable Panel. | U |
U to TS-CRYPTO 1.5.c (X1) & 1.5.g (X2) |
Initially UNCLASSIFIED. Special handling required. | |
h. Launch enable control group, Fig A 5034. | U |
U to TS-CRYPTO 1.5.c (X1) & 1.5.g (X2) |
Special handling required. | |
i. Launch commit key, operational and R&D. | U |
U |
Keys to panels in operational use will be controlled by at least two military members. | |
j. Cartridge tape unit. | U |
U or S 1.5.c (X1) |
UNCLASSIFIED only in situations such as disassembly where it is visually evident that the two classified printed circuit assemblies interface control module and drive control module have been removed | |
k. Amplifier, radio frequency, Fig A 9201. | U |
U |
R&D only. When tuned to classified frequency, classification will be the same as that of the frequency to which it is tuned. | |
l. Instrumentation group trainer test, guided missile Fig A 6370LW. | U |
U |
VAFB flight test only. MM III mod 7. | |
m. Instrumentation group trainer test, guided missile Fig A 6380. | U |
U |
VAFB flight test only. MM II mod 8 | |
8 | LCC Hardware | |||
a. Weapon System Processor (WSP) C0032102 | U |
U |
All WSP random access (volatile) memory (RAM) is dissipated when power is removed. The WSP is therefore UNCLASSIFIED when power is removed. Special handling required. | |
b. Bulk Storage/Loader (BS/L) C0032107 | U |
U or TS- FRD, (SIOP-ESI) Cat 6 and 10 1.5.g (X2) |
The hard disk assembly (HDA) is a removable hard disk. All weapon system control element (WSCE) executable software and databases are resident on the removable HDA. HDA becomes UNCLASSIFIED after successful overwrite. Overwrite procedure complies with CJCSI 3231.01. | |
c. Floppy Disk Drive, (FDD) C0032106 | U |
U or TS- FRD, (SIOP-ESI) Cat 6 and 10, 1.5.g (X2) |
Used in the console. Floppy disk drive does not retain classified information after power is removed. Diskettes installed in this drive become TOP SECRET - SIOP-ESI, unless the write protect tab is active during upload operations. If the write protect tab is not active, the information on the diskettes is classified. | |
d. Rapid Message Processor (RMP) CI 00200 | U |
U |
All RMP RAM memory is dissipated when power is removed. The RMP is therefore UNCLASSIFIED when power is removed. | |
e. RMP Backup Processor (RMPB) CI 00700 | U |
U |
All RMP Backup RAM memory is dissipated when power is removed. The RMP backup is therefore UNCLASSIFIED when power is removed. | |
f. Operator Input Device (OID) CI 032108 | U |
U |
Keyboard and trackball. Contains no memory. | |
g. Video Display Unit (VDU) CI 0032104 | U to TS- FRD, (SIOP-ESI) Cat 6 and 10 1.5.g (X2) |
U or TS- FRD, (SIOP-ESI) Cat 6 and 10 1.5.g (X2) |
VDU can display classified information and visual/physical access must be restricted IAW data being displayed. When turned off, visual/physical access is UNCLASSIFIED. No data retained in VDU when power is removed. | |
h. Printer, CI 0032105 | U or TS- FRD, (SIOP-ESI) Cat 6 and 10 1.5.g (X2) |
U or TS FRD, (SIOP-ESI) Cat 6 and 10 1.5.g (X2) |
Printed material can be classified and visual/physical access to printouts must be restricted IAW classification of printed data. Visual/physical access to the printer alone is UNCLASSIFIED. No data is retained in the printer when power is removed. | |
i. Coder-Decoder Assembly. (CDA) | U |
U |
Provides mounting and power supply for KI-22. The CDA itself is UNCLASSIFIED and retains no data. | |
9 | Operations Procedures Trainer Hardware | |||
a. Airborne Procedures Trainers (APT) Hardware | ||||
|
U |
U or TS 1.5.g (X2) |
Classification depends on information contained in the memory. Becomes UNCLASSIFIED when memory cleared with power off and disk pack removal. | |
|
U |
U or TS 1.5.g (X2) |
Disk packs may contain up to TOP SECRET data including training war plan information. UNCLASSIFIED when power and disk removed. | |
|
U or TS 1.5.g (X2) |
U or TS 1.5.g (X2) |
Classification depends on information contained in the memory. Becomes UNCLASSIFIED when memory cleared with power off and diskette removed. Diskettes may be classified up to TOP SECRET and contain training execution data. | |
|
U or TS 1.5.g (X2) |
U or TS 1.5.g (X2) |
Printed material may be classified and access to printouts must be restricted IAW classification of printed data. Visual/physical to the printer alone is UNCLASSIFIED. No data is retained in the printer when power is removed. | |
|
U |
U |
Used only by the computer operating system | |
|
U |
U |
||
|
U |
U |
||
|
U |
U |
||
|
U |
U |
||
|
U |
U |
||
|
U |
U |
||
|
U or TS 1.5.g (X2) |
U or TS 1.5.g (X2) |
May be classified TOP SECRET when in operation. UNCLASSIFIED otherwise. No memory. | |
|
U |
U |
Does not process classified information. | |
|
U or TS 1.5.g (X2) |
U or TS
1.5.g (X2) |
Printer material may be classified and access to printouts must be restricted IAW classification of printed data. Visual/physical to the printer alone is UNCLASSIFIED. No data is retained in the printer when power is removed. | |
|
U |
U |
||
b. Missile Procedures Trainers (MPT) Hardware Wg VI (LE) | ||||
|
U |
U or S 1.5.g (X2) |
Classification depends on information contained in the memory. Memory cleared with power off and disk pack removal. | |
|
U |
U or S 1.5.g (X2) |
Disk packs may contain SECRET data in the form of messages and systems parameters. UNCLASSIFIED when disk pack is removed. Declassify upon deactivation of WG VI unless needed for the NMD program. If needed for NMD, hardware will be reclassified under NMD guidelines. | |
|
U |
U or TS 1.5.g (X2) |
Classification depends on information contained in the memory. Becomes UNCLASSIFIED when memory cleared with power removal. | |
|
U |
U |
||
|
U or TS 1.5.g (X2) |
U or TS 1.5.g (X2) |
Classification depends on information contained in the memory. UNCLASSIFIED when memory cleared with power off and diskette removed. Diskettes may be classified TOP SECRET and contain training war plan data. | |
|
U to TS 1.5.g (X2) |
U to TS 1.5.g (X2) |
Printed material may be classified and access to printouts must be restricted IAW classification of printed data. Visual/physical access to the printer alone is UNCLASSIFIED. No data is retained when power is removed. | |
|
U |
U |
Used only by computer operating system. | |
|
U |
U |
Panels and switches, no computer functions. | |
|
U |
U |
Read-only simulator. Drives retain no data after power removal. | |
|
U |
U |
No memory or codes used. | |
|
U |
U |
Printed material may be classified and access to printouts must be restricted IAW classification of printed data. Visual/physical access to the recorder alone is UNCLASSIFIED. No data is retained when power is removed. | |
|
U or TS 1.5.g (X2) |
U or TS 1.5.g (X2) |
Printed material may be classified and access to printouts must be restricted IAW classification of printed data. Visual/physical access to the recorder alone is UNCLASSIFIED. No data is retained when power is removed. | |
|
U or S 1.5.g (X2) |
U or S 1.5.g (X2) |
May be classified TOP SECRET when in operation. UNCLASSIFIED when power off. No memory. | |
|
U or S 1.5.g (X2) |
U or S 1.5.g (X2) |
May be classified SECRET when in operation. UNCLASSIFIED when power off. No memory. | |
|
U |
U |
Panel and switches. No computer functions. No memory. | |
|
U |
U |
Panel and switches. No computer functions. No memory. | |
(17) Keyboard Printer
02-563002-5 |
U to TS 1.5.g (X2) |
U to TS 1.5.g (X2) |
Printed material may be classified and access to printouts must be restricted IAW classification of printed data. Visual/physical access to the recorder alone is UNCLASSIFIED. No data is retained when power is removed. | |
c. Missile Procedures Trainer Hardware | ||||
|
U |
U or TS 1.5.g (X2) |
UNCLASSIFIED when power off because processor memory does not retain data after removal of power. Processor contains TOP SECRET- data during operation with Removable Storage Element (RSE). | |
|
U |
TS 1.5.g (X2) |
RSE hard disk stores the MPT software including the MPTCP, MPTCOP, and EPP/MA database. | |
|
U |
TS 1.5.g (X2) |
Classification of the tape is dependent upon data that is archived to it. | |
|
U |
U |
Processor memory does not retain data after removal of power. | |
|
U |
U or TS 1.5.g (X2) |
Floppy disk drive does not retain classified information after power is removed. Floppy diskette remains UNCLASSIFIED if write protect tab is set during upload, otherwise the disketter assumes the highest classification of information in the system. | |
|
U or TS 1.5.g (X2) |
U or TS 1.5.g (X2) |
Printouts may be classified and visual/physical access to printout must be restricted IAW classification of printed data. Visual/physical access to the printer alone is UNCLASSIFIED. No data is retained after power off. | |
|
U or TS 1.5.g (X2) |
U or TS 1.5.g (X2) |
Visual/physical access must be IAW classification of displayed data. UNCLASSIFIED after power off, no data is retained. | |
|
U or TS 1.5.g (X2) |
U or TS 1.5.g (X2) |
Visual/physical access must be IAW classification of displayed data. UNCLASSIFIED after power off, no data is retained. | |
|
U or TS 1.5.g (X2) |
U or TS 1.5.g (X2) |
Visual/physical access must be IAW classification of displayed data. UNCLASSIFIED after power off, no data is retained. | |
|
U |
U |
Panel and switches, no computer functions. | |
|
U |
U |
Panel and switches, no computer functions. | |
|
U or TS 1.5.g (X2) |
U or TS 1.5.g (X2) |
Printouts may be classified and visual/physical access to printout must be must be restricted IAW classification of printed data. Visual/physical access to the printer alone is UNCLASSIFIED. No data is retained after power off | |
|
U |
U |
Panel and switches, no computer functions. | |
|
U |
U |
Panel and switches, no computer functions. | |
|
U |
U or TS 1.5.g (X2) |
UNCLASSIFIED after power off. TOP SECRET when diskettes are installed in this drive. | |
|
U |
U or TS 1.5.g (X2) |
UNCLASSIFIED after power off. Diskettes installed in this drive become TOP SECRET, unless the write protect tab is active during upload operations. | |
|
U |
U |
Panel and switches, no computer functions. | |
|
U |
U |
Panel and switches, no computer functions. | |
|
U or S 1.5.g (X2) |
U or S 1.5.g (X2) |
May be classified SECRET when in operation. UNCLASSIFIED when power off and thumbwheel switches normalized. No memory. | |
|
U |
U |
Panel and switches, no computer functions. | |
|
U |
U |
Simulator does not contain read/write head. Simulator contains optical device to detect presence of diskette. Drive retains no data after power removal. | |
|
U |
U to TS |
No attenuation provided by trainer enclosure. See AFI 31-209 | |
|
U |
U to TS DECLAS 31 Dec 2007 |
TEMPEST: No attenuation provided by trainer enclosure |
PROPULSION SUBSYSTEMS
Information Revealing |
Classification Reason Date |
Remarks |
|
1 | Complete design for Stages 1, 2, and 3 and the PSRE, not including hardness material associated with control units | U or S 1.5.g (X2) |
See Section XIV. |
2 | Physical characteristics for Stages 1, 2, and 3 and PSRE: | U |
|
a. Weight and mass properties | U |
Such as propellant, inert and total weights, center of gravity and moments of inertia. | |
b. Component material properties and characteristics, not including hardness materials associated with control units. | U |
See Section XIV. | |
3 | Solid propellant | U |
Such as formula, density, physical samples (cured or uncured), malfunctioning process or sensitivity to shock or fire. |
4 | Specific propulsion performance for Stages 1, 2, and 3 and PSRE | U |
Such as thrust action time, total or specific impulse, chamber pressure or combustion efficiency. |
5 | Thrust vector control, attitude control, roll control for Stages 1, 2, 3, and PSRE, not including information on hardness properties. | U |
Including actuation program, LITVC, delivered side forces, axial thrust augmentation or attitude control forces. See Section XIV. |
6 | Maintenance, repair and overhaul data and handbooks for Stages 1, 2, and 3, and PSRE. | U |
|
7 | Manufacturing process, tooling and gauges for Stages 1, 2, and 3, and PSRE. | U |
|
8 | Reliability of Stages 1, 2, and 3, and PSRE. | U to S 1.5.g (X2) |
UNCLASSIFIED unless the component (motor or PSRE) reliability is less than the propulsion subsystem reliability specification. CONFIDENTIAL if the component reliability is less than propulsion subsystem specification but greater than the system countdown and flight specification. SECRET if the component reliability is less than the system countdown and flight specification. |
9 | Vulnerability of Stages 1, 2, and 3, and PSRE to countermeasures. | S 1.5.g (X2) |
Hardness vulnerability, See Section XIV. |
MISSILE GUIDANCE SET (MGS) SUBSYSTEM
Information Revealing |
Classification Reason Date |
Remarks |
|
1 | Detailed design of complete subsystem | S 1.5.g (X2) |
Hardness vulnerability see Section XIV. |
2 | Specific performance of subsystem components and assemblies if such information reveals missile or subsystem operational capability or accuracy. | S 1.5.g (X2) |
See Section IV. For hardness vulnerability see Section XIV. |
a. G6B4 gyroscope | C to S 1.5.g (X2) |
G6B4 performance data by itself is considered CONFIDENTIAL. If associated with other inertial instruments it is considered SECRET. Data in EMDAS and MM Repair and Evaluation Data (RED) B portion of GO 78 is UNCLASSIFIED. | |
b. 16 PIGA MOD G accelerometer | C to S 1.5.g (X2) |
16 PIGA MOD G performance data by itself is considered CONFIDENTIAL. If associated with other inertial instruments it is considered SECRET. Data in EMDAS and MM REDB is UNCLASSIFIED. | |
c. GI-TI-B gyroscope | C to S 1.5.g (X2) |
GI-TI-B performance data by itself is considered CONFIDENTIAL. If associated with other inertial instruments it is considered SECRET. Data in EMDAS and MM REDB is UNCLASSIFIED. | |
d. Subsystem data available at repair depots | |||
|
U |
||
|
U |
||
|
U |
||
|
U |
||
|
U to S 1.5.g (X2) |
D37 hot channel data extracted prior to Overwrite is classified in accordance with other portions of this guide. Some classified data remains in the computer memory after Overwrite, and the D37 Hot Channel Protection Test or Mode 153. Data printed out by the depot configured software thereafter is unclassified. | |
|
U |
||
|
U |
||
3 | Reliability (NS-17, NS-20, NS-50) | ||
a. MGS (NS-17, NS-20 and NS-50). | U or S 1.5.g (X2) |
In-flight reliability of the MGS and its components is SECRET. | |
b. Components (Computer, GSP, MGSC, P92A3 downstage amplifier and downstage flight controls). | U or S 1.5.g (X2) |
See 3a comments. | |
c. Assemblies (D37 memory, G6B4 gyroscope, 16 PIGA Mod G accelerometer, GI-TI-B gyroscope). | U or S 1.5.g (X2) |
See 3a comments. | |
d. Subassemblies (Integrated circuits, and other related electronics). | U or S 1.5.g (X2) |
See 3a comments |
REENTRY SYSTEMS (RS)
The national policy on nuclear weapons dictates that only limited information
will be released. Specifically no authority exists to divulge, confirm
or deny the location at which special weapons are positioned, wherever they
are positioned. No questions will be answered regarding the employment
of nuclear weapons in a particular situation. The reply to questions
on authority to employ nuclear weapons will be authorized by the
President. In reply to inquiries, use of the terms thermonuclear and
hydrogen should not be used; atomic and nuclear should be avoided.
Replies should be phrased in such a way that they cannot be misconstrued
as gratuitous official pronouncements. Any unnecessary statements
concerning US nuclear-capable deterrent forces should be restrained.
In accordance with established policy, the US does not discuss the arms carried
by specific aircraft, vessels or other elements of its military forces and
avoids drawing attention to the need for conducting continuous military
operations with nuclear weapons. Certain US weapons systems have been
publicly identified as having a nuclear capability. This identification
does not in itself provide authority to release information concerning details
of storage, handling, or transportation of nuclear weapons or
components.
Except where noted, the following guidance applies, as applicable, to both
MM II and MM III.
Information Revealing |
Classification Reason Date |
Remarks |
|
1 | RVs: | U to TS-RD-CNWDI 1.5.g (X2) |
See RV guides. |
a. Association of an operational RS/RV with its nuclear warhead | |||
b. Fact that W56, W62, and/or W78 are thermonuclear weapons | |||
c. Warhead unit cost | See RV guides | ||
d. RV performance | See RV guides and Sections X and XIV | ||
e. Warhead yields | See RV guides and Sections X and XIV | ||
f. Target analysis studies | See RV guides and Sections X and XIV | ||
g. Height of Burst (HOB). Operational or test. | |||
|
See RV guides and Sections X and XIV | ||
|
See RV guides and Sections X and XIV | ||
h. Any other RV (warhead) information characteristics or performance | See RV guides and Sections X and XIV | ||
2 | Pen Aid systems: | ||
a. MM II | See Section XVII. | ||
b. MM III | |||
c. Hardening of Pen Aid systems. | See Section XIV, XVII, and XVIII. | ||
3. | RS: | ||
a. Administrative Information: | |||
|
U |
||
|
|||
|
U |
||
|
C 1.5.g (X2) |
||
|
See RV guides. | ||
|
S-FRD 1.5.g (X2) |
See subparagraph 3.a.(2) above. | |
|
S-FRD 1.5.g (X2) |
For additional information regarding Pen Aids, see Sections XVII and XVIII. | |
|
S-FRD 1.5.g (X2) |
||
|
U or C-FRD or S-FRD 1.5.g (X2) |
SECRET-FRD when W78 is identified as event source. CONFIDENTIAL-FRD is unannounced event is revealed. UNCLASSIFIED if W78 is not identified as the event source and only a planned or announced event is revealed. | |
|
U |
IAW TCG-WT-1 and TCG-WT-5 | |
|
U |
||
|
U |
||
|
U |
Except RV cost. See MK12 and MK12A guides. | |
b. Capability or performance information, actual or predicted: | See Section X, XVII, and XVIII. | ||
|
|||
|
S 1.5.g (X2) |
||
|
S-FRD 1.5.g (X2) |
||
|
S 1.5.g (X2) |
||
|
See RV guides | ||
|
S-FRD 1.5.g (X2) |
||
|
S 1.5.g (X2) |
See Sections XVII and XVIII | |
|
|||
|
S 1.5.g (X2) |
||
|
See RV guides | ||
|
|||
|
U |
See Sections XVII and XVIII | |
|
S 1.5.g (X2) |
||
|
S 1.5.g (X2) |
||
|
U |
||
|
See Section X item 4.h. and RV guides. | ||
|
S 1.5.g (X2) |
||
c. Physical properties | |||
|
Whether in person or via photos, drawings or sketches. | ||
|
U |
||
|
U |
||
|
U |
||
|
|||
|
See RV guides | ||
|
U |
Unclassified models, drawings, sketches, etc., shall not be made except for specific official requirements. Public release or display of unclassified photographs, etc., is not authorized. See RV guides. | |
|
U to S 1.5.g (X2) |
See item 3.c.(3)(c) below. | |
|
U to S-FRD 1.5.g (X2) |
Use the most restrictive single or combined applicable guidance from 3c(1)(b)1. thru 3. above. | |
|
|||
|
See RV guides | ||
|
See RV guides | ||
|
|||
|
S-FRD 1.5.g (X2) |
||
|
See RV guides | ||
|
See RV guides | ||
|
U |
||
|
U |
||
|
U to S 1.5.g (X2) |
See Sections XVII and XVIII. | |
|
|||
|
|||
|
S-RD CNWDI 1.5.g (X2) |
||
|
U |
||
|
U |
||
|
U |
||
|
U |
||
|
U |
||
|
U |
||
|
U |
||
|
C-FRD 1.5.g (X2) |
MK12A RS | |
|
U |
||
|
U |
||
|
|||
|
See RV guides | ||
|
See RV guides | ||
|
|||
|
U to S 1.5.g (X2) |
See Sections XVII and XVIII. | |
|
S 1.5.g (X2) |
See Sections XVII and XVIII. | |
d. Design Details: | |||
|
U |
||
|
For RV telemetry, see RV guides. For Mod 7/8 see Section X. | ||
|
U to S-FRD 1.5.g (X2) |
Refer to applicable subsections of this Guide and the appropriate RV guide. | |
|
|||
|
S to S-RD 1.5.g (X2) |
Refer to applicable subsections of this Guide and the appropriate RV guide. May be FRD or RD depending upon information revealed. | |
|
U to S-FRD 1.5.g (X2) |
Refer to applicable subsections of this Guide and the appropriate RV guide. | |
|
U to S-FRD 1.5.g (X2) |
Refer to applicable subsections of this Guide and the appropriate RV guide. | |
|
U to C-FRD 1.5.g (X2) |
UNCLASSIFIED when IOC date has been officially released. CONFIDENTIAL-FRD for MK12A until IOC date has been released by DOD. | |
|
C-FRD 1.5.g (X2) |
See this Guide and MK12A Guide | |
|
See RV guides | ||
|
See RV guides | ||
|
See RV guides | ||
|
See RV guides | ||
|
See RV guides | ||
|
See RV guides | ||
|
|||
|
U |
||
|
S to TS-FRD 1.5.g (X2) |
Refer to applicable subsections of this Guide and the appropriate RV guide. | |
|
See RV guides. | ||
e. Operational data: | |||
|
|||
|
U |
||
|
U |
||
|
S-FRD 1.5.g (X2) |
||
|
U |
Except for special missions. | |
|
U or S 1.5.g (X2) |
The number and/or location of operational missiles with pen aids for more than one wing or 150 missiles is classified SECRET. | |
f. PBV flight data predicted or actual at any time after Stage 3 thrust termination: | NOTE: If vulnerability to countermeasures or a method of discrimination is revealed, HQ AFSPC/DOM approval for release or dissemination is required. | ||
|
U to S-FRD 1.5.g (X2) |
Real time radar and telemetry data measured and recorded by test range instrumentation is UNCLASSIFIED until processed. When such data is subsequently processed or analyzed, it will be classified IAW the provisions of this Guide. Specifically, all MM booster trajectory data up to thrust termination is UNCLASSIFIED. For classification of data after thrust termination, refer to the appropriate RV guide. Post launch analysis and trajectory reconstruction will be classified SECRET-FRD if precise target location, World Geodetic System (WGS), coordinates are derived and/or depicted. Analysis of abnormal/anomalous trajectory will be classified IAW this Guide. | |
|
S-FRD 1.5.g (X2) |
See RV guides. | |
|
S-FRD 1.5.g (X2) |
See RV guides. | |
|
S-FRD 1.5.g (X2) |
See RV guides. | |
|
S-FRD 1.5.g (X2) |
See RV guides. | |
|
See RV guides. | ||
|
S-FRD 1.5.g (X2) |
See RV guides. | |
|
S-FRD 1.5.g (X2) |
See RV guides. | |
|
U |
||
|
S U 1.5.g (X2) |
See RV guides. | |
|
|||
|
S 1.5.g (X2) |
||
|
S-FRD 1.5.g (X2) |
See RV guides. | |
|
S-FRD 1.5.g (X2) |
See RV guides. | |
|
S-FRD 1.5.g (X2) |
See RV guides | |
|
S-FRD 1.5.g (X2) |
See RV guides | |
|
|||
|
U |
||
|
S 1.5.g (X2) |
||
|
S-FRD 1.5.g (X2) |
See RV guides | |
|
S-FRD 1.5.g (X2) |
See RV guides | |
|
|||
|
See RV guided | ||
|
See RV guides | ||
|
S-FRD 1.5.g (X2) |
See RV guides | |
|
TS-FRD 1.5.g (X2) |
See RV guides | |
|
C-FRD 1.5.g (X2) |
See RV guides | |
|
S-FRD 1.5.g (X2) |
See RV guides | |
|
S-FRD 1.5.g (X2) |
See RV guides | |
(5) Exoatmospheric point mass. | S 1.5.g (X2) |
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IMPROVED MINUTEMAN PHYSICAL SECURITY SYSTEM (IMPSS)
SECURITY AUXILIARY SYSTEM
Unclassified information that pertains to security measures, including plans,
procedures and equipment, for the physical protection of Special Nuclear
Material (SNM) where unauthorized dissemination could have a significant
adverse effect on public safety, the common defense and security due to illegal
production of nuclear weapons, or the theft, diversion or sabotage of SNM
should be considered for protection as DOD UCNI. Material originated
prior to dissemination of DOD UCNI interim procedures that is found in the
normal course of business to contain UCNI will be protected as UCNI.
There is no requirement to conduct detailed files searches to retroactively
identify UCNI. However, as unclassified information pertaining to the
physical protection of SNM is withdrawn from file, it should be reviewed
to determine if it meets the criteria for protection as UCNI (and marked
accordingly).
Information Revealing |
Classification Reason Date |
Remarks |
|
1 | Complete design of the security subsystem | U or S 1.5.g (X2) |
The hardware design is UNCLASSIFIED. Complete software design is SECRET. The secret aspects of the software design are: The outer zone (OZ) amplitude and phase alarm threshold constants; The OZ time of integration constants; the inner zone (IZ) amplitude alarm threshold constants; and, the IZ time of integration constants. Other software components are UNCLASSIFIED. |
2 | Schematic drawings or manufacturing drawings: | U or S 1.5.g (X2) |
SECRET if the system/subsystem probability of detection for a human intruder using any penetration mode or technique is revealed or can be deduced. SECRET if a system/subsystem vulnerability is revealed or can be deduced. The OZ subsystem outer and inner range gate size is UNCLASSIFIED if no probability of detection information is revealed. |
a. R&D analyses/tradeoff studies | U |
||
3 | Reliability data | U |
|
4 | False/nuisance alarm rate data | U |
|
a. R&D analyses/tradeoff studies | U |
||
5 | Maintenance requirements and procedures | U or S 1.5.g (X2) |
See Item 2. remarks. |
6 | Subsystem vulnerability: | S 1.5.g (X2) |
Any information that reveals a system vulnerability is SECRET. |
a. Detection limitation. | S 1.5.g (X2) |
See Item 2. remarks. | |
b. Possible methods of degrading system performance that would not be identified by the Nuclear Safety Certification or system self check | S 1.5.g (X2) |
SECRET if the plots or patterns of system detection sensitivity are drawn to scale and are labeled with probability of detection information. Plots or patterns of area of coverage with no information relative to system probability of detection are UNCLASSIFIED. | |
7 | Plots or patterns of security system area of coverage with respect to actual or simulated human penetration | U or S 1.5.g (X2) |
See Item 6.b. remarks |
8 | Transmitter frequency. | U |
|
9 | Power output. | U |
|
10 | Signal processing techniques. | 1.5.g (X2) |
SECRET when system sensitivity can be deduced. The signal processing techniques are SECRET if they reveal or introduce a subsystem vulnerability (i.e., the differential side-band processing technique is UNCLASSIFIED). |
a. R&D analyses/tradeoff studies | U |
||
11 | False/nuisance alarm event. | U |
|
12 | Subsystem life. | U |
|
13 | Complete listing of operational subsystem software. | S 1.5.g (X2) |
See Item 1. remarks. |
14 | Partial listing of the operational subsystem software. | U or S 1.5.g (X2) |
See Item 1. and 2. remarks. |
15 | Development of test software. | U or S 1.5.g (X2) |
See Item 2. remarks. |
16 | Test results and analysis a. Raw test data not relating to potential system design/performance |
S - U 1.5.g (X2) |
Classified related to detection thresholds, patterns, or vulnerabilities. If not related to the above, UNCLASSIFIED. Unclassified if not related to detection thresholds, patterns or vulnerabilities. |
17 | OZ filter integration times. | S 1.5.g (X2) |
See Item 1. remarks |
18 | IZ integration time. | S 1.5.g (X2) |
See Item 1. remarks. |
19 | Military application | U |
|
20 | Latch-up time | U |
|
a. R&D analyses/tradeoff studies | U |
||
21 | Reset time | U |
|
22 | Circuit design thresholds for alarm | S 1.5.g (X2) |
|
23 | Frequency of drawer self check. | U |
|
24 | System probability of detection. | S 1.5.g (X2) |
|
25 | Detection limitations relative to target velocity. | S 1.5.g (X2) |
The detection limitations relative to target velocity are SECRET if they reveal or introduce a subsystem vulnerability. |
26 | Physical security system hardware | ||
(1) Receiver Transmitter alarm set P/N 25-90426-1, -3 (CI 1514AA) | U or S 1.5.g (X2) |
Visual access UNCLASSIFIED. Review security measures for possible protection as UNCI. Receiver transmitter alarm set drawer is SECRET when processor P/N 21-61925 with PROMS P/N 21-61699-33, 34, 35, 36, or 38, 39, 40,41 are installed. If PROMS are not installed, the processor card and drawer are UNCLASSIFIED | |
(a) Circuit card assembly processor, A2 P/N 21-61699-5 | U or S 1.5.g (X2) |
Visual access UNCLASSIFIED. Physical access SECRET when PROMS P/N 21-61699-33, 34, 35, 36, or 38, 39, 40, 41 are installed. If PROMS are removed the A2 circuit card is UNCLASSIFIED | |
1. Programmable Read Only Memory (PROM) anti-intrusion alarm set operational software (CI 1516AA). | S 1.5.g (X2) |
P/Ns 21-61699-33, 34, 35, 36. | |
(2) Antenna assembly, (C1015151AA) | U |
P/N 25-799-50-4 | |
27 | Development or production hardware. | U or S 1.5.g (X2) |
Any development hardware or firmware that functionally or electrically represents the system baseline design, or production hardware or firmware that, when analyzed, reveals detection sensitivity or reveals a system/subsystem vulnerability is SECRET. The external view of any hardware is UNCLASSIFIED. |
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LAUNCH FACILITY PERSONNEL ACCESS AUXILIARY SYSTEM
Information Revealing |
Classification Reason Date |
Remarks |
|
1 | Design criteria | S 1.5.g (X2) |
TO 21M-LGM30F-2-19 contains unclassified procedures. Applicable classified data is contained in TO 21M-LGM30F-4-1-2. Drawings which show the location of the secondary door (Fig A 1604) in the locked position are classified SECRET. |
2 | Specifications. | U |
TO 21M-LGM30F-2-19 contains unclassified procedures. Applicable classified data is contained in TO 21M-LGM30F-4-1-2. Drawings which show the location of the secondary door (Fig A 1604) in the locked position are classified SECRET. |
3 | Schematic diagrams: | ||
a. Entire security and alarm system, secondary door and security pit vault door circuits. | S 1.5.g (X2) |
||
b. Individual end items. | U |
TO 21M-LGM30F-2-19 contains unclassified procedures. Applicable classified data is contained in TO 21M-LGM30F-4-1-2. Drawings which show the location of the secondary door (Fig A 1604) in the locked position are classified SECRET. | |
4 | Design information: | ||
a. Penetration resistance. | S 1.5.g (X2) |
||
b. Time configuration. | S 1.5.g (X2) |
||
c. External configuration | U |
||
d. Internal details. | S 1.5.g (X2) |
TO 21M-LGM30F-2-19 contains unclassified procedures. Applicable classified data is contained in TO 21M-LGM30F-4-1-2. | |
5 | Maintenance and operating requirements and procedures. | S 1.5.g (X2) |
TO 21M-LGM30F-2-19 contains unclassified procedures. Applicable classified data is contained in TO 21M-LGM30F-4-1-2. |
6 | Drawings: | ||
a. System. | S 1.5.g (X2) |
Drawings which show the location of the secondary door (Fig A 1604) in the locked position are classified SECRET. | |
b. Manufacturing. | S 1.5.g (X2) |
TO 21M-LGM30F-2-19 contains unclassified procedures. Applicable classified data is contained in TO 21M-LGM30F-4-1-2. | |
7 | Total quantities. | U |
TO 21M-LGM30F-2-19 contains unclassified procedures. Applicable classified data is contained in TO 21M-LGM30F-4-1-2. |
8 | Reliability. | U |
|
9 | Hardware | ||
a. Security pit vault door (Fig A 1608). | |||
|
S 1.5.g (X2) |
||
|
U |
Provided the combination has been removed and IZ alarm switch loops are disconnected. | |
|
U |
||
|
U |
Provided the combination has been removed and IZ alarm switch loops are disconnected. | |
b. Secondary door (Fig A 1604): | |||
|
S 1.5.g (X2) |
||
|
U |
Provided the combination has been removed and IZ alarm switch loops are disconnected. |
AIRBORNE LAUNCH CONTROL SYSTEM (ALCS)
AUXILIARY SYSTEM
Also see Worldwide Airborne Command Post System (WWABNCP) Security Classification
Guide.
Information Revealing |
Classification Reason Date |
Remarks |
|
1 | That an ALCS is being used. | U |
|
2 | Design and performance characteristics | U |
UNCLASSIFIED unless information regarding the cryptologic is revealed. COMSEC Controlled Item. |
a. If information regarding the crypto logic is revealed. | S-CRYPTO 1.5.g (X2) |
COMSEC Controlled Item. | |
3 | Overall force hardness and survivability resulting from ALCS. | TS-FRD 1.5.g (X2) |
|
4 | Method of operation of control unit and groups (Stations 1, 2, and 3). | U |
|
5 | Operational ALCC-Wing data frequencies. | U |
|
6 | ALCS codes: | Also see USSTRATCOM SD 501-12 | |
a. Operational launch codes: | |||
|
U |
||
|
TS-CRYPTO 1.5.c (X1) |
||
b. Test codes: | |||
|
U |
||
|
S-CRYPTO 1.5.c (X1) |
||
7 | ALCS auxiliary system: | ||
a. Code Processor Equipment
Fig A 1990, TSEC/K1-45 |
U to TS-CRYPTO 1.5.c (X1) |
Visual access UNCLASSIFIED. S to TS-CRYPTO Controlled COMSEC Item TOP SECRET-CRYPTO with operational cryptovariable installed. Special control handling, and classification required. DECLAS according to applicable COMSEC document/guidance | |
b. KIK-45/TSEC Volatile keying assembly | U to S 1.5.c (X1) |
Visual access UNCLASSIFIED. Controlled COMSEC Item. One KIK-45 holds half the KI-45 key. Used with USKAU/USKMU. TOP SECRET - CRYPTO with operational codes installed DECLAS according to applicable COMSEC documents/guidance. | |
c. USKAU -100 A/B keying variable assembly | U or TS-CRYPTO 1.5.c (X1) |
Visual access UNCLASSIFIED. Controlled COMSEC Item. Used with KSK-45 DECLAS according to applicable COMSEC documents/guidance. | |
d. USKMU-100 A/B | U to S-CRYPTO 1.5.c (X1) |
Visual access UNCLASSIFIED. Controlled COMSEC Item. Used with KSK-45 DECLAS according to applicable COMSEC documents/guidance. | |
e. Special purpose cryptographic keyer KSK-45 | U to S 1.5.c (X1) |
Visual access UNCLASSIFIED. Controlled COMSEC Item. Used to transfer the keying variable into the KIK-45. Controlled COMSEC Item. Used with KSK-45. DECLAS according to applicable COMSEC documents/guidance. | |
f. Power supply | U |
||
g. Transmitter control | U |
||
h. Input/Output unit | U |
||
i. Receiver groups | U |
||
j. Control unit stations 1, 2, and 3 | U |
||
k. Group ÂAÂ kits (cabling, bracketing, harness, etc). For aircraft installation. | U |
||
l. Components for communication assemblies used including frequencies. | U |
||
m. Tapes (ALCS) | See Section XIX | ||
8 | Reliability data: | ||
a. ALCS | S 1.5.g (X2) |
||
b. Airborne system, ALCC | C 1.5.g (X2) |
||
c. Ground system. | C 1.5.g (X2) |
Individual components not classified by other sections of this Guide are UNCLASSIFIED; however, any compilation of data which may indicate a trend or rate will be classified as indicated above | |
9 | Parts, accessories, subassemblies and equipment available in the open market or produced for commercial use if classified use is not revealed. | U |
|
10 | Vulnerability information. | S 1.5.g (X2) |
|
11 | Impact of ALCS on operational capabilities. Wing or Force. | Classify per other guidance in this guide | |
12 | Initial operational readiness dates (ALCS): | ||
a. Airborne system. | U |
||
b. Ground systems (Wing). | U |
||
13 | Aircraft | U |
|
a. Total number modified for ALCS | U |
||
b. Master schedule for modification. | U |
||
14 | Documents relating to training programs at Air Force or contractor facilities | Classified according to contents as determined by this guide. |
COMMUNICATIONS - ELECTRONICS
Higher authority communications terminals used in the Minuteman Weapon System
to provide connectivity to the National Command Authority and other higher
authorities may have performance parameters, modulation, signal processing,
error correction, timing, and other characteristics that are classified.
The applicable communications system security classification guide should
be consulted for classification determination of specific system
characteristics.
Information Revealing |
Classification Reason Date |
Remarks |
|
1 | Design and specification of the voice telephone, interphone, and radio systems. | U |
|
2 | Design of the radio overlay control component. | U |
|
3 | Wire system specifications, wire layout and pair count. | U |
|
4 | Wire system field surveys. | U |
|
5 | Command control receiver. | U |
|
6 | MF radio launch control system (WS-133B only): | ||
a. Generalized basic and background data. | U |
||
b. General frequency band of operation | U |
||
c. Specific operational frequencies. | U |
||
d. General antenna characteristics | U |
||
7 | Generalized information on jamming | U |
No details. No frequencies or frequency ranges. No specific techniques. |
8 | Code requirements document. | S 1.5.c (X1) |
|
9 | Details of mechanical-electrical generation of codes. | S 1.5.c (X1) |
|
10 | General information on code formats | U |
Provided no calibration information, frequencies or formats are revealed. See USSTRATCOM SD 501-12 |
11 | Hardness of operational sites. | See Section XIV. | |
12 | Specific anti-jam features or techniques | S 1.5.c (X1) |
Includes detailed drawings which reveal classified data. System characteristics if such information reveals limitations or design. |
13 | Anti-jam test data | S 1.5.c (X1) |
|
14 | Launch codes: | ||
a. Complete operational launch code. | TS-CRYPTO 1.5.c (X1) |
Special handling required IAW USSTRATCOM SD 501-12. . | |
b. Partial operational launch code. | S to TS-CRYPTO 1.5.c (X1) |
More than half of the launch code is TOP SECRET-CRYPTO. | |
c. Launch enable codes | S to TS-CRYPTO 1.5.c (X1) |
See USSTRATCOM SD 501-12 for TOP SECRET-CRYPTO. | |
d. Test launch codes | U |
||
15 | Command destruct frequencies | Test codes are unclassified unless specified otherwise by NSA or the COMSEC supplement to the Industrial Security Manual. | |
a. Command destruct receiver frequency range. | U |
||
b. Sequencing logic required to trigger destruct. | U |
||
16 | Reliability | U or S 1.5.g (X2) |
SECRET when reliability data is lower than weapon system reliability requirements. |
17 | Transattack/postattack communications availability and limitations. | S 1.5.g (X2) |
Could reveal system vulnerabilities for exploitation. |
TESTING PROGRAM
The purpose of this section of the Guide is to establish the classification
of information generated in preparation for, in support of, or as a result
of flight and ground test operations. Flight test operations are herein
defined to include Development Test and Evaluation (DT&E) and Operational
Test and Evaluation (OT&E) flight tests. Ground test operations
are defined to include operational ground test programs such as, but not
limited to, Simulated Electronic Launch Minuteman (SELM) where a modification
to the weapon system or a subset of the weapon system is being evaluated
without having missile flight as an objective. In some instances, there
may be a repetition of data presented in other sections of this Guide, but
this was done intentionally to include all data pertinent to the testing
community in one section of this Guide. The classification guidance
presented in this section is intended for flight test systems that are prepared
and launched on the national test ranges as well as for ground tests conducted
in the operational force, at Vandenberg AFB or Ogden ALC test facilities.
It is not intended to contradict or override the classifications assigned
to operational deployed systems. Depending on the configuration of
the missile and the potential involvement of different Associated Operations
on HQ AFSPC MM test launches, different RV and Associated Operation program
Security Classification Guides may apply. Review the missile configuration
and list of approved Associated Operations from HQ AFSPC/DO for each mission
(Glory Trip) to determine which other classification guides apply.
Information Revealing |
Classification Reason Date |
Remarks |
|
1 | Weapon system testing program: | Except warheads or warhead mockups. | |
a. The fact that nonstandard payloads are flown on HQ AFSPC OT&E missions. | U |
This is a general statement. Items 1.c., d., and e. must be reviewed for applicability for each program. | |
b. The fact that a nonstandard payload was flown on a specific HQ AFSPC OT&E mission (i.e., identifying Glory Trip # or WSMC Op #). | U to S 1.5.g (X2) |
TBD by classification of the Associated Operation Program or by HQ AFSPC/DOM. | |
c. Association of the sponsoring agency name, an unclassified program name or descriptive identifier (e.g., Infrared Imaging System) with HQ AFSPC in general. | U to TS 1.5.g (X2) |
TBD by classification of the Associated Operation Program and notified by HQ AFSPC/DOM. | |
d. Association of an unclassified program name or descriptive identified (e.g., Infrared Imaging System) with HQ AFSPC OT&E). | U to TS 1.5.g (X2) |
See Item 1.c remarks. | |
e. Association of an unclassified program name or descriptive identifier (e.g., Infrared Imaging System) with a specific HQ AFSPC OT&E mission. | U to TS 1.5.g (X2) |
An example is associating program name with Glory Trip # or WSMC Op #. See Item 1.c. remarks | |
f. Specific requirements for any associated operation will be handled in accordance with appropriate classification guides SCGs and/or supplemented by program security guidance issued by HQ AFSPC. | U to TS 1.5.g (X2) |
NOTE: For Items 1.c., d., and e., the classification of the association may be downgraded to UNCLASSIFIED after each mission is flown. TBD by classification of the Associated Operation Program and notified by HQ AFSPC/DOM. | |
g. Information pertaining to anomalies discovered during developmental testing of a system/subsystem. | U to TS-RD 1.5.g (X2) |
If the same anomaly exists or can be expected to exist and adversely affect the performance of any current operational system, the data will be classified as directed in the appropriate section of this Guide. Public utility furnished adjuncts and interfaces are exempted from classification. | |
h. OT&E (flight tests, SELM tests) and other designated ground tests such as Olympic Plays. | U to S 1,5,g (X2) |
The fact that an Olympic Play or SELM anomaly occurred is UNCLASSIFIED.
For SELM anomalies, the specific anomaly is classified until determination
can be made of possible force wide implications
For Olympic Play testing anomalies, less than 10 failures in one squadron are UNCLASSIFIED. Failure modes at higher rates are classified until determination can be made of possible force wide implications. Reports describing these failures are also with classified or unclassified based on the squadron failure rates depicted in them. EMDAS data and reports are unclassified. Failure rates and descriptions from more than one wing are classified SECRET. |
|
|
S 1.5.g (X2) |
General objectives not identifying performance or design specifications criteria are UNCLASSIFIED | |
|
S-FRD 1.5.g (X2) |
||
|
S 1.5.g (X2) |
Results/conclusions/analyses or reports indicating causes or possible causes of test failures/anomalies including specific failed components will be classified SECRET until it can be proven that there is no force-wide impact on weapon system capability, vulnerability, limitations, accuracy or reliability. The determination of force-wide impact and the decision to declassify or upgrade applicable data will be made by HQ AFSPC/DOT prior to reclassifying the data. | |
|
U |
With no clarification. | |
|
S 1.5.g (X2) |
Every effort must be made to protect the identification of the failure/anomaly cause or possible cause including specific failed weapon system components as SECRET unless the revelation is required for safety purposes. Western Test Range flight data will be processed and classified in the same manner whether or not a weapon system anomaly/failure occurred. Final reports derived from the test range data will be classified SECRET. | |
|
S to TS-RD 1.5.g (X2) |
See Section XIII and remarks in 1.h.(3) and 1.h.(3)(b) above. | |
|
See RV guides | ||
|
S 1.5.g (X2) |
||
|
See Section XIII and remark in 1.h.(3) above. | ||
|
See Section XIV | ||
|
Sure-kill vulnerabilities normally concern nuclear hardness and/or Pen Aids. See Section XIV, XVII, and XVIII. | ||
|
S 1.5.g (X2) |
||
|
See RV guides | ||
|
TS-FRD 1.5.g (X2) |
||
|
|||
|
U |
||
|
|||
|
See RV guides | ||
|
S 1.5.g (X2) |
||
|
U |
For example, program schedules and complete missile test schedules for entire test program. | |
|
U |
For example, planned HQ AFSPC operational flight test dates. For public disclosure, see Section II (Administrative Details). | |
|
U or S 1.5.g (X2) |
UNCLASSIFIED when World Geodetic System (WGS) coordinates for the LF are not provided. SECRET when WGS coordinates are provided. | |
|
U |
||
|
U |
||
|
U |
||
|
U to TS-FRD 1.5.g (X2) |
Includes all magnetic visicorder charts, test conductor logs, etc. See Section III (Performance Data). | |
|
U |
See Section III (Performance Data). | |
|
U |
Real time radar and telemetry data measured and recorded by test range instrumentation is UNCLASSIFIED until processed. When such data is subsequently processed or analyzed, it will be classified IAW the provisions of this Guide. Specifically, all MM booster trajectory data up to thrust termination is UNCLASSIFIED. For classification of data after thrust termination, refer to the appropriate RV guide. Post launch analysis and trajectory reconstruction will be classified SECRET-FRD if precise target location, WGS, coordinates are derived and/or depicted. Analysis of abnormal/anomalous trajectory will be classified IAW this Guide. | |
|
U |
||
i. Missile target range. | U |
Distance to test range. See 1.h. above. | |
j. Target location: | |||
|
S-FRD 1.5.g (X2) |
||
|
U |
To an accuracy not closer than one nautical mile. | |
k. Booster trajectory: | |||
|
S 1.5.g (X2) |
See Section XIII. | |
|
C 1.5.g (X2) |
||
|
U |
||
|
U |
Refer to appropriate RV guides where TMIG is post-thrust termination. | |
l. RV reentry angle azimuth. | U |
Operational Test Launches only. See RV guides. | |
m. Range azimuth envelope and missile alignment. | U |
For example, launch time, azimuth and site location (if no WGS coordinates are indicated). | |
n. Range azimuth limits. | U |
||
o. Specific launch azimuth | U |
||
p. Telemetry: | |||
|
U |
Unless they reveal classified aspects of the system being measured. | |
|
S 1.5.g (X2) |
If they reveal classified aspects of the system being measured. | |
|
|||
|
U to C 1.5.g (X2) |
See Section III (Performance Data) and appropriate RV guide. | |
|
U to S-FRD 1.5.g (X2) |
See Section III (Performance Data) and appropriate RV guide. | |
|
U |
For example, number of words per frame, number of frames per second and sampling. | |
|
U |
When calibration information and test data are together and will reveal classified information on the weapon system, it is classified by this Guide according to the information revealed | |
|
U |
See para 4. for classification of missile performance information. | |
|
U |
Provided information requiring classification by para 1.p.(3)(a) or (b) above is not revealed. | |
|
U to S-RD to TS-FRD 1.5.g (X2) |
See para 4 of this Section for classification of missile performance information. | |
q. Telemetry frequencies: | |||
|
U |
||
|
U |
||
2 | Operational test launch history reports showing only success or failure: | ||
a. A single operational test history report when an indication of failure or test objectives and/or details of the results are shown. | C to TS-RD 1.5.g (X2) |
May be CONFIDENTIAL to TOP SECRET-RD when otherwise required by this Guide depending upon information revealed. This applies to para 1.h. | |
b. A compilation of two or more operational test launch history reports when an indication of failure of test objectives and/or details of the test results are shown. | C to TS-RD 1.5.g (X2) |
See remarks 2.a. above. | |
3 | Special tests | Governed by classification guidance provided for that specific test. | |
4 | Missile performance test data: | ||
a. Specific performance of propulsion subsystems (Stages 1, 2, or 3) | See Section III. | ||
b. Specific performance of PBV. | S to TS-FRD 1.5.g (X2) |
If sequencing and or deployment of Pen Aids to RVs is revealed (Includes PSRE performance which requires classification of the guides, such as the MK 12 Guide). See Sections IV, XVII, and XVIII for subsystem performance classification requirements or applicable RV guide. TOP SECRET only if specific vulnerability is revealed. | |
c. G&C subsystem performance | S 1.5.g (X2) |
When such information reveals missile or subsystem operational capability or limitations, i.e., accuracy, vulnerability, etc. See Section XIII. | |
d. RV performance | See appropriate RV guide. | ||
e. Pen Aids performance | See Sections XVII and XVIII. | ||
f. PSRE performance. | U to S 1.5.g (X2) |
See Section III. | |
g. Test launch narration: | |||
|
|||
|
U |
||
|
S-FRD 1.5.g (X2) |
See Section V and RV guides | |
h. Weapon system accuracy, predicted or actual: | Measured in Circular Error Probable (CEP). The CEP is defined as the radius of a circle, centered about the aimpoint, within which 50 percent of the RVs are expected to impact. (Sometimes referred to as miss distances). | ||
|
S-FRD 1.5.g (X2) |
For either individual launches or any compilation of launches. | |
|
See appropriate RV guide | ||
|
S 1.5.g (X2) |
See remark in para 4.h. above. | |
|
|||
|
See appropriate RV guide | ||
|
See appropriate RV guide | ||
i. Uprange optical data: | MM II or III | ||
|
U or S or S-FRD 1.5.g (X2) |
See remarks in 1.h.(3). Nonanomalous uprange video at the time of TT is UNCLASSIFIED. | |
|
See remarks in 1.h.(3). Low light level TV data from WSMD AN/ASQ-145 (gunship) sensors is SECRET-FRD | ||
|
S-FRD 1.5.g (X2) |
||
|
S-FRD to TS-FRD 1.5.g (X2) |
Classify SECRET-FRD until evaluation determination is made. If evaluation finds that a Pen Aids vulnerability is detectable, upgrade film to TOP SECRET-FRD | |
5 | Other tests: | Excluding flight tests but including status, short duration and subscale tests. | |
a. Test directives. | Classified according to content as determined by this Guide. | ||
b. Test results and conclusions. | Classified according to content as determined by this Guide. | ||
c. Dates of individual tests | U |
With or without test number and unclassified test objectives. | |
d. Location of tests, including test stand designation. | U |
||
e. Significant progress on/or completion of major objectives in the test program | UNCLASSIFIED provided classified design or performance parameters are not revealed | ||
6 | In-place survivability testing. | In-place survivability test information will be classified in accordance with Section XIV. | |
7 | Test data pertaining to RV. | See RV guides. |
OPERATIONAL GROUND EQUIPMENT (OGE)
Information Revealing |
Classification Reason Date |
Remarks |
|
1 | Ground handling and support equipment, test equipment, training equipment or programs, instrumentation (internal and external), maintenance, repair and overhaul (as contained in handbooks, etc.) reentry and penetration program. | U to S-RD 1.5.g (X2) |
See applicable sections of this guide. |
2 | All terminal equipment other than operational coding equipment for communications-electronics. | U |
|
3 | Launch Control System for WingsÂI, III, V, VI. | U to TS-CRYPTO 1.5.g (X2) |
When the Status Authentication System equipment drawers are installed in the Launch Control System, SECRET-CRYPTO; when operational launch and inhibit codes are inserted in Launch Control System, TOP SECRET-CRYPTO; otherwise UNCLASSIFIED. See Section II. Also see USSTRATCOM SD 501-12 |
4 | All terminal equipment other than operational coding equipment for communications-electronics | U |
|
5 | OGE and/or production schedules. | U |
See Section XIII |
6 | Reliability | U or S 1.5.g (X2) |
If no equipment or system performance or CRYPTO information requiring classification by other sections is revealed. SECRET if survival period reliability or OGE strategies alert reliability can be determined. |
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FACILITIES
Information Revealing |
Classification Reason Date |
Remarks |
|
1 | Views of the LF and/or MAF. | U |
|
2 | LFs and MAFs: | If hardness is revealed, see Section XIV. | |
a. Plans and specifications for construction contract purposes. | U |
Unless locations of and/or design "hardness" modifications are identified therein, then classify according to other sections of this Guide. | |
b. The number of LFs and/or MAFs | U |
Not under "Operational Readiness." | |
c. Maintenance requirements and procedures. | U |
||
d. Type of configuration for a squadron upon completion of construction. | U |
Example: 5X10, i.e., 5 LCCs with 10 launchers per LCC. | |
3 | LF and MAF subsurface conditions: | ||
a. Information which discloses the geological subsurface conditions existing at a specific LF or MAF. | U or S 1.5.g (X2) |
Information providing complete dynamic test results of subsurface geologic conditions which allow the determination of ground motion from a nuclear blast at a LF or MAF is SECRET. | |
b. Information which discloses the geological subsurface conditions for the general area in which a flight, squadron or wing is located. | U |
||
c. Information which correlates an LF or MAF attack response to a specific geological subsurface condition. | S to TS 1.5.g (X2) |
Responses at an individual LF or MAF are classified SECRET; responses allowing a qualitative force assessment by squadron or wing are TOP SECRET. | |
4 | Documents related to training programs at Air Force or contractor facilities. | Classified according to contents as determined from this Guide. | |
5 | Load and stresses resulting from missile emplacement and launches that launchers are designed to withstand. | U |
|
6 | General performance of Real Property Installed Equipment (RPIE). | U |
Information does not reveal the operational limitations or capabilities of the facility. |
7 | Reliability. | U or S 1.5.g (X2) |
SECRET is survival period reliability can be determined. |
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SECTION XIII
OPERATIONAL DATA
Information Revealing |
Classification Reason Date |
Remarks |
|
face="Times" size="1"> | face="Times" size="1"> | face="Times" size="1"> | face="Times" size="1"> |
1 | Operational capability date for additions to the ICBM force and/or planned operational readiness dates of individual squadrons | S 1.5.g (X2) |
The operational force date is defined as the officially planned date by which a given operational force is tactically deployed under the operational control of an operating command. |
2 | The total number of missiles in HQ AFSPC that are committed to the SIOP at any point in time: | S 1.5.g (X2) |
|
a. The number of ICBMs in HQ AFSPC that are on alert at the current time. | U |
||
3 | Weapon system reaction time. | S 1.5.g (X2) |
Weapon system reaction time is the time required to launch any number of missiles; this should not be confused with preplanned commit or delay times which are classified by GATI (Generation and Targeting Instructions) |
a. Planned reaction time for any one or more squadrons of an operational force. | U |
||
b. Demonstrated reaction time for any one or more squadrons of an operational force. | U |
||
4 | Number of MM missiles planned or authorized for: | ||
a. The ICBM force: | U |
||
b. A tactical squadron | U |
||
c. The total number of MM III missiles for the entire MM force. | U |
||
d. Number of MM III missiles for a specific MM wing, squadron or flight. | U |
||
5 | Actual rates of delivery of MM missiles to the ICBM force. | U |
|
6 | Location of operational force support bases. | U |
|
7 | Geodetic, astronomic and geometric parameters required for publication of the missile launch site data catalog: | ||
a. The following classification directives apply to Point X and Point A geodetic, astronomic and gravimetric parameters. | Point X and Point A were locations used for early MM targeting procedures | ||
|
U or S 1.5.g (X2) |
UNCLASSIFIED when given to no better than the closest minute. | |
|
|||
|
C 1.5.g (X2) |
||
|
U |
||
|
C 1.5.g (X2) |
||
|
U |
||
|
S 1.5.g (X2) |
||
|
U |
||
|
U |
||
|
C 1.5.g (X2) |
||
b. Parameters when given to no better than closest minute. | U |
||
c. The following classification directives apply to any permanent marker employed in determining requisite parameters for Point X and Point a. | |||
|
C 1.5.g (X2) |
Except coordinates rounded to the nearest one-tenth of a minute or worse. | |
|
U |
||
|
U |
||
|
|||
|
C 1.5.g (X2) |
||
d. The following classification directives apply to statements of parameter accuracy requirements and parameter accuracies achieved: | |||
|
C 1.5.g (X2) |
||
|
U |
||
e. Other pertinent materials. | C 1.5.g (X2) |
Classification policy for other pertinent materials, e.g. WGS, 1972 transformation formulas, will be coincident with Defense Mapping Agency Technical Report, ìDepartment of Defense World Geodetic System 1972 (U), Ãà 1 Jan 1974. | |
f. Parameter accuracy requirement and/or the accuracy data published on the MISDS. | S 1.5.g (X2) |
When revealed in conjunction with the effects on MM subsystem performance classify SECRET. The relationship of geodetic, astronomic, and gravimetric parameters errors and/or uncertainties to subsystem or to total weapon system performance that reveals operational capability or limitations will be classified SECRET. | |
8 | Complete concept of weapon system employment | S 1.5.g (X2) |
May be RD or FRD. See RV guides. The term ìconceptî includes associating Pen Aids with their mission. See Sections XVII and XVIII. |
9 | Official weapon system command control and communications plan for operational units. | S 1.5.g (X2) |
|
10 | Preliminary target system and priority recommendations. | S 1.5.g (X2) |
|
11 | Target system and priorities based on USAF war plans. | TS 1.5.g (X2) |
|
12 | Preliminary estimates of weapon system capabilities and effectiveness. | S 1.5.g (X2) |
May be RD or FRD. See RV guides. |
13 | Weapon system capabilities and effectiveness based on USAF war plans. | TS 1.5.g (X2) |
May be RD or FRD. See RV guides. |
14 | Location of Alternate Command Post (ACP). | U |
|
15 | Target selection capability (the number of targets a missile may select): | ||
a. Of the missile alone: | U |
||
b. When coupled with other missile capabilities. | S 1.5.g (X2) |
The term ìother missile capabilitiesî specifically includes associated Pen Aids with their mission. See Section XVII and XVIII. | |
16 | Operational mode periods. | The time duration that the System is expected to operate in the indicated operational mode. | |
a. Normal mode | U |
Normal operation on commercial power. | |
b. Standby AC mode | S 1.5.g (X2) |
Diesel generated ac power. Operating requirements such as, total operating time or extended survival operating time are SECRET. | |
c. Survival mode periods: | The time periods under specified attack environments that missiles could still be launched successfully. | ||
|
The required time period prior to launch and under specified attacks that the system will operate on emergency (batteries) power. | ||
|
S 1.5.g (X2) |
||
|
S 1.5.g (X2) |
||
|
S 1.5.g (X2) |
The required time period under specified attacks that the system will operate on extended survival power. | |
|
|||
|
S 1.5.g (X2) |
||
|
S 1.5.g (X2) |
||
|
S 1.5.g (X2) |
||
|
S 1.5.g (X2) |
Survival period reliability refers to strategic alert reliability during the survival period. | |
17 | Target azimuth when associated with the location or designation of the LF. | S 1.5.g (X2) |
|
18 | Target azimuth not associated with the location or designation of the LF. | U |
|
19 | Launch azimuth not associated with the location or designation of the LF. | U |
|
20 | Autocollimation positioning azimuth for Safeguard System Test Target Program (SSTTP) flights. | U |
|
21 | Firing order | S 1.5.g (X2) |
Sequence in which missiles would be fired in an operational flight. |
22 | External configuration of the MM missile. | U |
|
23 | Fig ìAî or CI list | Classified according to the nature of the equipment and/or content, as determined from this Guide. | |
24 | Force Modernization/Force Improvement Programs | U |
Schedules disclosing planned deployment/delivery dates for modifications to the MM Program are UNCLASSIFIED except when classification is required by the classification guide covering the modified hardware (MK12A, etc.) |
25 | Weight data of stages or the assembled missile (less RS). | U |
See Section V and RV guides |
26 | Complete design of missiles (less RS). | S 1.5.g (X2) |
See Section V and RV guides |
27 | Specific military performance, planned or actual. | U to S-FRD 1.5.g (X2) |
See RV guides and appropriate sections of this Guide. |
28 | General performance. | U |
Such as ìintercontinental rangeî, ìsupersonic reentryî but excluding performance generalities about impact speed. |
29 | Specific performance of MM missile. | U to S-FRD 1.5.g (X2) |
See RV Guides and Section X of this Guide |
30 | Estimate or proven conclusions as to weapon system capability or operational limitations. | S to TS-RD 1.5.g (X2) |
See Section X, Section III (Performance Data) and Section XIV. |
31 | Vulnerability of the MM weapon system to countermeasures proven or unproven: | ||
a. LFs and MAFs | S to TS 1.5.g (X2) |
For hardness, see Section XVII | |
b. MM missile. | S to TS 1.5.g (X2) |
See RV guides and appropriate sections of this Guide. May be RD or FRD if nuclear weapon information is revealed. | |
32 | Handbook of Weight and Balance data | C 1.5.g (X2) |
|
33 | Reliability: | ||
a. Weapon System | S or S-FRD 1.5.g (X2) |
Reliability data of RV is SECRET-FRD. See RV guides | |
b. Missile | S to S-FRD 1.5.g (X2) |
||
c. Weapon system strategic alert, countdown or flight reliability | S 1.5.g (X2) |
||
d. Strategic alert reliability of operational ground equipment | S 1.5.g (X2) |
||
34 | Command control: | ||
a. Command control receiver package | U |
||
b. Assigned operational frequency. | U |
||
35 | Location of RV/payload | The term ìLocationî refers to the fact of existence of the RV/payload at a given location or in a specified area of LF. The term ìRV/payloadî refers to any MM-related RV, warhead, nuclear weapon or payload whether it is war reserve, operational or a training item. This includes MK12, MK12A, W56, W62, 78 (all types) payloads, both operational and training. See para 36 below for more guidance. Full consideration of Appendix III of the AF Security Classification Guide for Nuclear Weapons has already been taken. | |
a. Training RV/Payload: | |||
|
Such as MK11 Type 3/3A, W62 Type 3, etc. | ||
|
U |
||
|
U or C-FRD 1.5.g (X2) |
Classify as if a WR item. See RV guides | |
|
U |
||
b. Location of WR or operational RV/payload | U |
||
|
U |
The location of MM sites standing nuclear alert is UNCLASSIFIED. However, national policy is that the presence of nuclear weapons, at any location, will neither be confirmed nor denied. Therefore, extreme caution must be exercised when making public statements or comments to nongovernment personnel. | |
|
U |
National policy is that the presence of nuclear weapons at any location will neither be confirmed nor denied. Therefore, extreme caution must be exercised when making public statements or comments to nongovernment personnel. | |
|
Classify at the highest level, as appropriate, listed below. | ||
|
U to S-FRD 1.5.g (X2) |
Classify locations and planned primary and alternate convoy routes IAW AFI 31-101 series regulations. | |
|
U to S-FRD 1.5.g (X2) |
Classify locations and planned primary and alternate convoy routes IAW AFI 31-101 series regulations. | |
|
C-FRD 1.5.g (X2) |
See RV Guides and AF SCG for Nuclear Weapons. | |
36 | Quantities of RVs/payloads | See Remark for paragraph 35 above for definition of ìRVs/payloads.î | |
a. All MM units | |||
|
S-FRD 1.5.g (X2) |
See topics 1571, 1533, 1560-63 and 1573 of CG-W-4, Joint ERDA/DOD Nuclear Classification Guide for additional guidance. | |
|
S-FRD 1.5.g (X2) |
See Remark 36.a.(1) above. | |
37 | Operation Readiness Inspection (ORI) evaluation results. | U |
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SECTION XIV
NUCLEAR HARDNESS & SURVIVABILITY (NH&S)
Due to sensitivity of ICBM nuclear hardness, survivability, and vulnerability,
the following procedures will be applied to all classification levels of
hardness information:
Information Revealing |
Classification Reason Date |
Remarks |
|
1 | General | ||
a. Nuclear weapon effects studies or the fact that nuclear weapons effects are being studied. | U to TS to TS-RD/FRD 1.5.g (X2) |
Requires special guidance from HQ AFSPC/DOMN for each circumstance | |
b. System hardness | |||
|
U |
This specific information has been officially released. | |
|
U to TS-RD/FRD 1.5.g (X2) |
For RV hardening, see RV guides. Requires special guidance from HQ AFSPC/DOMN for each circumstance. | |
|
U |
This specific information has been officially released. | |
c. Hardness impacts and discrepancies: | Hardness impacts may affect mission critical functions. | ||
|
U to TS RD/FRD 1.5.g (X2) |
Requires special guidance from HQ AFSPC/DOMN for each circumstance. Declassification would reveal vulnerabilities to assist in the use of weapons of mass destruction. | |
|
S-RD/FRD to TS-RD/FRD 1.5.g (X2) |
Declassification would reveal vulnerabilities to assist in the use of weapons of mass destruction SECRET - RD if relating to the design or fabrication of weapons and FRD if external characteristics, including size, weight and shape, yields and effects, and systems employed in the delivery or use thereof. TOP SECRET - RD if impact on survivability is related to the design or fabrication of weapons, and FRD if external characteristics, including size, weight and shape, yields and effect, and systems employed in the delivery or use thereof, and if survivability of similar configuration (e.g., wing, force) can be inferred. | |
|
S 1.5.g (X2) |
Declassification would reveal vulnerabilities to assist in the use of weapons of mass destruction. | |
|
U |
||
|
S 1.5.g (X2) |
If mission completion is jeopardized, treat as a hardness impact in accordance with para 1.c.(1) above. | |
d. Hardness design criteria: | |||
|
S or S-RD/FRD 1.5.g (X2) |
Examples are numerical specifications that reveal the extent of protection provided against each particular nuclear effect. SECRET RD if quantified in terms related to criteria for nuclear weapons effects. | |
|
U |
||
|
U/S 1.5.g (X2) |
If relationship to design criteria or threat criteria is given or supplied, refer to paraÂ(1.d.(1). If any Hardness qualification or acceptance test levels reveal ground shock environment for hard mounted or shock isolated subsystems/components refer to paragraph (1) and paragraph (2) (will be classified SECRET). | |
e. Design considerations/materials: | |||
|
U to C-RD to S-RD-CNWDI 1.5.g (X2) |
UNCLASSIFIED if material is normally used in a nonhardened design application, and the hardening application is not specifically referred to. Normally, and unless classified information is revealed, material, shielding, or hardening techniques used against all effects except X-Ray are UNCLASSIFIED in generic texts. The design of special materials for X-Ray hardening is CONFIDENTIAL-RD. The fact of use of special materials by name or type for X-Ray hardening is also CONFIDENTIAL-RD. (per -WT-1) SECRET-RD if materials are described or identified for X-Ray hardening. SECRET-RD (CNWDI) if nuclear weapon design information is revealed. | |
|
U |
||
|
U |
Except when revealed in conjunction with hardness levels. See para 6.b. | |
f. RS hardening materials. | C-RD to S-RD 1.5.g (X2) |
See para 1.e.(1) above. | |
g. Funding requirements for proposed or approved hardness or survivability program. | U or S 1.5.g (X2) |
SECRET if changes in hardness levels can be inferred. | |
h. Planning and schedule | U or S 1.5.g (X2) |
Complete planning, programming or scheduling for any proposed or approved hardness activity. SECRET if changes in hardness levels are defined or can be inferred. | |
2 | Weapon system ground facilities: | ||
a. General information. | U or S to TS-RD/FRD 1.5.g (X2) |
Refer to para 1. | |
b. Nuclear weapons effects testing. | U or S to S-RD/FRD 1.5.g (X2) |
Refer to para 5. | |
c. Assessment: | |||
|
U or S to TS-RD/FRD 1.5.g (X2) |
Refer to para 6. | |
|
TS-RD/FRD 1.5.g (X2) |
These are quantitative statements of assessed hardness, distinct from vulnerability statements. | |
d. Endurability: | Except as otherwise noted, endurable hardness equipment and survivability information will be classified as launch-essential/mission-critical weapon system ground facilities hardness and survivability information | ||
|
S 1.5.g (X2) |
SECRET if hardness level or hardness design level is revealed. | |
|
S (X2) |
The time period that the system will remain operational on Emergency (battery) or Extended Survival (battery and diesel generator) power | |
3 | Missile: | ||
a. G&C: | U or S 1.5.g (X2) |
||
|
U or S 1.5.g (X2) |
UNCLASSIFIED if the level of environment is not specified. | |
|
S -RD-FRD or TS-RD-FRD 1.5.g (X2) |
SECRET if the level of environment is specified. See 1.c. (1).(a) above. | |
b. Pen Aids | |||
|
U to S-RD |
See para 1.e. (1) above | |
c. RS: | |||
|
|||
|
U |
||
|
U |
See para 1.b. | |
|
U to S 1.5.g (X2) |
Requires special guidance from HQ AFSPC/DOMN for each circumstance. | |
|
C-RD to S-RD 1.5.g (X2) |
See para 1.e (1) above. | |
|
S-RD 1.5.g (X2) |
Visual access is UNCLASSIFIED when appearance does not disclose use of the material. A part number on or associated with an item discloses use and is therefore classified SECRET-RD. | |
|
C 1.5.g (X2) |
||
|
S-RD 1.5.g (X2) |
||
|
C-RD or S-RD 1.5.g (X2) |
SECRET-RD if design level of hardness is revealed. | |
|
C-RD or S-RD 1.5.g (X2) |
SECRET-RD if design level of hardness is revealed. | |
d. Nuclear weapons effects testing. | U or S-RD/FRD 1.5.g (X2) |
Refer to para 5. | |
e. Assessed hardness, survivability or vulnerability | U to TS-RD/FRD 1.5.g (X2) |
Refer to para 6. | |
4 | Communications system: | ||
a. Communications equipment: | Includes all receivers, transmitters, and antennas or connectors collocated with the weapon system. | ||
|
U to TS-RD/FRD 1.5.g (X2) |
Refer to para 1. | |
|
U or S-RD-FRD 1.5.g (X2) |
Refer to para 5. | |
|
U to TS-RD-FRD 1.5.g (X2) |
Refer to para 6. | |
b. Connectivity: | Refers to message transmission paths not collocated with and not part of the weapon system. | ||
|
U to TS-RD/FRD 1.5.g (X2) |
Requires special guidance from HQ AFSPC/DOMN for each circumstance. | |
|
U to TS-RD/FRD 1.5.g (X2) |
Requires special guidance from HQ AFSPC/DOMN for each circumstance. | |
5 | Nuclear weapons effects testing: | Encoding provisions of para 6.b.(3) apply. Testing may be of a weapon system unique component, which is a part, subassembly, drawer rack or subsystem manufactured or configured in such a way as to be unavailable to the general public; or testing may be of a generic component, which is a part, subassembly, drawer, rack, or subsystem which is either a) regularly used for other than Government purposes, or b) is available for purchase or trade to non-Government entities or the general public. As a general rule, test information, including fragility levels, of a generic component is easily reproducible by other organizations and is UNCLASSIFIED. | |
a. Tester performance: | |||
|
U |
Test levels at test equipment interfaces are not classified unless information requiring classification by other provisions of this Guide are revealed | |
|
S 1.5.g (X2) |
||
|
S-RD/FRD 1.5.g (X2) |
||
b. Test configuration. | U |
Includes physical test data and configuration drawings, including test measurement, which do not reveal hardness design criteria or nuclear weapons effects criteria. Test levels by themselves are not classified unless their relationship to the specification hardness levels is stated or implied. | |
c. Calibration data. | U or S 1.5.g (X2) |
SECRET when data reveals information from which hardness design criteria can be deduced | |
d. Weapon system test data/ results: | Including measured test responses; excluding tester performance data. | ||
|
U |
Generic components include (but are not limited to) integrated circuits, transistors, silicon controlled rectifiers, diodes and other electronic piece-parts. UNCLASSIFIED if the annotation does not reveal any potential impact and test predictions do not state their relationship to any classified criteria levels. | |
|
S to S-RD/FRD 1.5.g (X2) |
Weapon system unique components include tailored electrical circuits, modules, drawers, subsystems, and overall system. SECRET-RD when related to restricted data RD criteria levels. | |
|
U or S to S-RD/FRD 1.5.g (X2) |
UNCLASSIFIED for generic components if the relationship of test levels to specification hardness levels is not stated or implied. SECRET for weapon system unique components. SECRET-RD when related to RD critical levels. If damage is incurred, see para 5.e. | |
|
U or S to S-RD/FRD 1.5.g (X2) |
UNCLASSIFIED if the relationship of test levels to specification hardness levels and potential impacts is not stated or implied. SECRET-RD when related to RD criteria levels. | |
|
U |
Annotated data is data which 1) identifies or implies use of the tested item in the weapon system either by part number (or other weapon system unique identifier) or by stating use or location, and 2) identifies the tested parameter(s) or test condition(s). UNCLASSIFIED if the relationship of test levels to specification hardness levels and potential impacts is not stated or implied. | |
|
S to S-RD/FRD 1.5.g (X2) |
Refer to para 5.d.(2) above, and para 5.e. | |
|
U |
UNCLASSIFIED subject to the provisions of Section III (Performance Data). | |
|
U |
||
|
U |
UNCLASSIFIED if hardness design criteria, nuclear effects criteria, and/or level at which any item being tested failed is not revealed. | |
|
U or S 1.5.g (X2) |
UNCLASSIFIED if the level are not related to hardness levels. | |
e. Test fragilities: | |||
|
U |
See para 6.b.(3) | |
|
U or S to S-RD/FRD 1.5.g (X2) |
UNCLASSIFIED if levels are not related to specification hardness levels. | |
|
S to S-RD/FRD 1.5.g (X2) |
See para 5.d.(6) and 6.b.(3). | |
|
U or S to S-RD 1.5.g (X2) |
See para 5.d.(6) and 6.b.(3). | |
f. Test survivability. Inferred probability of survival of weapon system unique components under nuclear environments simulated by testing. | S 1.5.g (X2) |
If overall weapon system survivability is affected, see para 1.c.(1).(a). | |
6 | Assessment: | ||
a. Threats and environments: | |||
|
S to S-RD/FRD 1.5.g (X2) |
SECRET-RD if weapon design criteria can be obtained. | |
|
S-RD/FRD 1.5.g (X2) |
||
|
U to S-RD/FRD 1.5.g (X2) |
SECRET-RD if weapon design criteria can be obtained. | |
|
U or S to S-RD/FRD 1.5.g (X2) |
UNCLASSIFIED if levels are not related to hardness environment levels. SECRET- RD if weapon design criteria can be obtained. | |
b. Assessed hardness or fragility levels: | Hardness levels are assumed to affect critical mission accomplishment. | ||
|
TS-RD/FRD 1.5.g (X2) |
Official hardness assessment will be made only as directed by the Chief of Staff, USAF. The release or dissemination of any assessment data will be by HQ AFSPC/DOMN. | |
|
TS-RD/FRD 1.5.g (X2) |
See remarks in para 6.b.(1) above. | |
|
U or S to S-RD/FRD 1.5.g (X2) |
UNCLASSIFIED if component and function in the weapon system is not referred to and the hardness environment levels can not be derived. SECRET if potential mission consequences of failure are given or can be inferred. SECRET-RD if related to RD criteria levels | |
|
S or S-RD/FRD or TS-RD/FRD 1.5.g (X2) |
TOP SECRET-RD if assessed system hardware level can be inferred and quantified in terms related to weapon criteria & if hardness or fragility levels of similar configurations (e.g. wing, force) can be inferred. | |
|
U |
UNCLASSIFIED if the guidelines of para 6.b.(3) above are used to classify the code document | |
c. Threat responses from predictions and assessments: | |||
|
S to S-RD/FRD 1.5.g (X2) |
SECRET-RD if related to RD criteria levels. | |
|
U |
UNCLASSIFIED if responding equipment, location in the weapon system, and mission-critical function are not revealed. Code documents must be classified IAW guidance in this section. | |
|
S to S-RD/FRD 1.5.g (X2) |
Direct-coupled responses are not to be coded. SECRET-RD if related to RD criteria levels. | |
|
S or S-RD/FRD or TS-RD/FRD 1.5.g (X2) |
See paragraph 6.b. | |
|
U |
UNCLASSIFIED if hardness environment levels can not be derived. | |
|
U to TS-RD/FRD 1.5.g (X2) |
Upset/Recovery times UNCLASSIFIED if mission completion is not jeopardized. | |
d. Assessed survivability: | |||
|
TS-RD/FRD 1.5.g (X2) |
Official survivability assessment will be made as directed by the Chief of Staff, USAF. The release or dissemination of any survivability data will be by HQ AFSPC/DOM. | |
|
S to TS-RD/FRD 1.5.g (X2) |
Classify IAW appropriate paragraphs within this section on weapon system threat responses and fragility levels used to derive the survivability distribution | |
|
U |
Distribution parameters are UNCLASSIFIED if distribution means or survivability or other critical tolerance limits are not revealed. | |
|
S 1.5.g (X2) |
||
|
S to S-RD/FRD 1.5.g (X2) |
SECRET-RD if levels are expressed which reveal restricted data criteria. | |
e. Vulnerability | The term vulnerability usually refers to operation in a hostile environment rather than in a benign environment. The term includes susceptibility to fragment or projectile penetration, nuclear radiation, blast loadings, RF transmissions, etc. | ||
|
For RV vulnerability see RV guides | ||
|
S to S-RD/FRD 1.5.g (X2) |
If countermeasure environments specify nuclear criteria characteristics, then SECRET-RD. | |
|
S to TS - RD/FRD 1.5.g (X2) |
SECRET if demonstrated vulnerability is for one missile. TOP SECRET if vulnerability is for more than one missile. | |
|
|||
|
S-RD/FRD 1.5.g (X2) |
Technology to include nuclear weapons effects criteria. See RV guides | |
|
U to TS or TS-RD/FRD 1.5.g (X2) |
UNCLASSIFIED if status is Partial Mission Capable (PMC) for individual or combined facilities. SECRET if application is to a single strategic missile, MAF or LF. TOP SECRET if application can be extended to similar configurations, such as squadron, wing, MM II or III missile, or entire force. TOP SECRET-RD if vulnerability is to criteria nuclear weapons effects. | |
f. Criticality. | C 1.5.g (X2) |
Criteria for mission criticality of hardened components or subsystem, expressed in terms of mission consequences. |
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SYSTEM SAFETY FAULT TREE ANALYSIS RESULTS
Information Revealing |
Classification Reason Date |
Remarks |
|
1 | Results of fault tree analysis probability IND, FL, and AMI.IPL | S-FRD 1.5.g (X2) |
For example: Probability of AMI is
10-xx per squadron in ten years. |
2 | That fault tree analysis is being accomplished to determine the probability of: | ||
a. Faulty Launch (FL) | U |
||
b. Inadvertent Nuclear Detonation (IND) | U |
||
c. Accidental Motor Ignition (AMI) | U |
||
d. Inadvertent Programmed Launch IPL) | U |
||
3 | The specification level numerical probability that must be met: | ||
a. Faulty Launch (FL) | U |
Fault tree analysis are UNCLASSIFIED if the values (numbers) are not included. | |
b. Inadvertent Nuclear Detonation (IND) | U |
Fault tree analysis are UNCLASSIFIED if the values (numbers) are not included. | |
c. Accidental Motor Ignition (AMI) | U |
Fault tree analysis are UNCLASSIFIED if the values (numbers) are not included. | |
d. Inadvertent Programmed Launch (IPL) | U |
Fault tree analysis are UNCLASSIFIED if the values (numbers) are not included. | |
4 | The actual or calculated numerical probability: | ||
a. Faulty (FL) | S 1.5.g (X2) |
To include Fault Tree formats to support development | |
b. Inadvertent Nuclear Detonation (IND) | S-FRD 1.5.g (X2) |
To include Fault Tree formats to support development | |
c. Accidental Motor Ignition (AMI) | S 1.5.g (X2) |
To include Fault Tree formats to support development | |
d. Inadvertent Programmed Launch (IPL) | S 1.5.g (X2) |
To include Fault Tree formats to support development | |
5 | Results of fault analysis identifying the probability of: | The preferred format is: The Probability of AMI or IND etc. is 10-xx (super script) per squadron in XX years. | |
a. Faulty Launch (FL) | S 1.5.g (X2) |
To include Fault Tree formats used to support development. | |
b. Inadvertent Nuclear Detonation (IND) | S-FRD 1.5.g (X2) |
To include Fault Tree formats used to support development. | |
c. Accidental Motor Ignition (AMI) | S 1.5.g (X2) |
To include Fault Tree formats used to support development. | |
d. Inadvertent Programmed Launch (IPL) | S 1.5.g (X2) |
To include Fault Tree formats used to support development. |
SECTION XVI
UNAUTHORIZED LAUNCH
AND
LAUNCH ACTION STUDIES
Information Revealing |
Classification Reason Date |
Remarks |
|
1 |
A compilation of unauthorized launch (UL) scenarios of any WS-133 system covering multiple areas of vulnerabilities. | TS 1.5.g (X2) |
Basic or revised studies for each weapon system configuration. |
2 |
A single complete UL scenario with detailed procedures. | TS 1.5.g (X2) |
|
3 |
A single or compilation UL scenario(s) limited to a single area of vulnerability but not revealing detailed procedures. | S 1.5.g (X2) |
Such as studies for modifications when an addendum is written. |
4 |
Partial UL scenario(s). | S 1.5.g (X2) |
Usually during UL Study preparation or in briefings. |
5 |
Detailed procedures for accomplishing a portion of an UL scenario or information revealing a system or component vulnerability. | S 1.5.g (X2) |
|
6 |
A complete launch action study with detailed procedures. | S 1.5.g (X2) |
|
7 |
A partial launch action study with detailed procedures. | C to S 1.5.g (X2) |
Dependent upon extent of detail in the launch action study. Classify per special guidance from AFSC/SEW for each case. |
8 |
A complete launch action study without detailed procedures but revealing a component vulnerability | C 1.5.g (X2) |
|
9 |
A partial launch action study without detailed procedures and not revealing a component vulnerability. | U |
|
10 |
That UL studies and launch action studies exist. | U |
|
11 |
Vulnerabilities to communication security keys, codes or algorithms. | TS 1.5.g (X2) |
Applies to all systems using nuclear command and control. |
Note: Access to these documents is strictly controlled by AFSC/SEW. AFI 91-106 Unauthorized Launch and Launch Action Studies is the controlling directive and provides information on authorized access, preparation, use of cover sheets, and storage requirements and distribution and destruction restrictions.
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MM II PEN AIDS (MK I/MK IA PEN AIDS)
Information Revealing
Classification
Reason
Date
Remarks
Even though it has been phased out, MK I Pen Aids system information remains classified due to its similarity with the MK IA Pen Aids system. 1 Use of acronyms or abbreviations. Classify the same as the information that would be revealed if not abbreviated. 2 Complete engineering. U or S
1.5.g (X2)
MK I or MK IA subsystem engineering or operational mock-ups. UNCLASSIFIED when Pen Aids Countermeasure System (PACS) units are not included 3 Pen Aids spacer. S
1.5.g (X2)
Visual access is UNCLASSIFIED 4 Mating details of Pen Aids: a. Element with canister S
1.5.g (X2)
An element is any dipole or reflector carried within the Pen Aids canister.
- b. Canister with spacer.
S
1.5.g (X2)
This subject concerns any information detailing the orientation of the canister within the launch tubes and their positioning in the dispersal sequence. c. Spacer with missile U
A spacer is the structural section which contains the canisters and ordnance. 5 Data on minor hardware and ordnance items from which internal canister details, mating details or RV position in clouds cannot be determined U
6 Payload information revealing: a. Type of Pen Aid payload such as chaff, wire, exhaust plume, etc. S
1.5.g (X2)
b. Total number of Pen Aid canisters carried. U to S
1.5.g (X2)
SECRET: Individual operational sortie. c. Number of salvos or number of Pen Aids per salvo. S
1.5.g (X2)
A salvo describes the dispersal of the Pen Aids canisters. A salvo may consist of one or more chaff puffs ejected at one time. 7 Infrared signature S
1.5.g (X2)
8 Existence of a threat cloud or threat tube. U
9 Threat cloud size, density or pattern S
1.5.g (X2)
10 In-flight spacing or accuracy of spacing. S
1.5.g (X2)
11 Screening: a. Type or extent. S
1.5.g (X2)
b. Dispersion operating rates and survival altitude. S
1.5.g (X2)
c. Altitude of ejection. S
1.5.g (X2)
d. Operational flight characteristics or performance. S
1.5.g (X2)
e. System reliability. S
1.5.g (X2)
f. Signature characteristics:
- (1) Radar frequency band
S
1.5.g (X2)
- (2) Radar cross section.
S
1.5.g (X2)
- (3) Reflective or response frequencies
S
1.5.g (X2)
- (4) Any other signature characteristics
S
1.5.g (X2)
12 Type of enemy radar encountered; e.g., range or frequency band. S
1.5.g (X2)
13 Specific vulnerability information for subsystems or components TS
to
TS-RD
1.5.g (X2)
14 Specific and detailed information on countermeasures or protection from enemy countermeasures. TS
to
TS-RD
1.5.g (X2)
15 Pen Aids flight test and performance information. Evaluation of operational Pen Aids performance against design requirements or postulated threat. S
or
TS-FRD
1.5.g (X2)
16 Known or suspected anomalies and possible relationship to MM II force-wide impact. S
or
TS-FRD
1.5.g (X2)
17 Flight test times and locations. U
18 Production data. U or S
1.5.g (X2)
19 Manufacturing data. S
1.5.g (X2)
20 Chaff (whether or not identified as such):
- a. Visual access to external package assembly (with or without ejection device).
U
b. Dipoles, wire, etc:
- (1) Material (generic title).
C
1.5.g (X2)
- (2) Prior to cutting to desired lengths.
C
1.5.g (X2)
- (3) Diameter
C
1.5.g (X2)
- (4) Lengths
S
1.5.g (X2)
21 The MK11 RV position in chaff train on any test mission. S-FRD
1.5.g (X2)
22 Association of MM II Pen Aids with their mission. S
1.5.g (X2)
See Section XIII.
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SECTION XVIII
MM III PEN AIDS (MK12/MK12A PEN AIDS)
PART A
COMPLETE PEN AIDS SYSTEM
Information Revealing
Classification
Reason
Date
Remarks
1 Any association or cross association of the terms, MM III, MK12, MK12A RS, MK12/MK12A Pen Aids, chaff, decoys or dipoles. U
2 Pen Aids production data: a. Total quantities to be produced or contracted for. U
b. Planned or actual rates of delivery to any operational site S
1.5.g (X2)
The number of RVs or decoys postured on or planned for any operational missile is SECRET-FRD. c. Funding U
or
S-FRD
1.5.g (X2)
SECRET-FRD if War Reserve RVs (WR RV) quantities can be determined 3 Number of chaff dispensers per operational missile. S
1.5.g (X2)
4 Pen Aid system reliability. S
1.5.g (X2)
5 Targeting accuracy of Pen Aids system S
1.5.g (X2)
6 Maximum or minimum range of Pen Aids system. S
1.5.g (X2)
7 Vulnerability to countermeasures. TS
1.5.g (X2)
If vulnerability to countermeasures or a method of discrimination is revealed, HQ AFSPC/DO approval for release or dissemination is required 8 Missile discrete or analog signal characteristics (voltage and duration of signal) used to initiate events or control Pen Aids components U
or
S-FRD
1.5.g (X2)
When total number of signals is revealed, SECRET-FRD. 9 DC power allotment or utilization of Pen Aids system. U
10 Trajectory information: a. Exoatmospheric point mass S
1.5.g (X2)
b. Exoatmospheric dynamic trajectories S
1.5.g (X2)
c. Reentry trajectories. S-FRD
1.5.g (X2)
See RV guides. 11 Mission sequence of Pen Aid events including timing and deployment altitudes. S
1.5.g (X2)
12 Evaluation of operational Pen Aids performance against design requirements or postulated threats S
or
TS-FRD
1.5.g (X2)
TOP SECRET-FRD if a method of discrimination is revealed, HQ AFSPC/DOM approval for release or dissemination is required. If vulnerability to countermeasures or a method of discrimination is revealed, HQ AFSPC/DO approval for release or dissemination is required. 13 Hardening of MK12/MK12A Pen Aids U
or
S-FRD
1.5.g (X2)
See Sections V and XIV. 14 Number of chaff reentry trains U
or
S-FRD
1.5.g (X2)
UNCLASSIFIED for Operational Test (OT) missiles, otherwise SECRET-FRD. 15 Geometry of reentry train. a. Train to train distances. S-FRD
1.5.g (X2)
b. Cloud to cloud distances. S-FRD
1.5.g (X2)
16 Known or suspected anomalies and possible relationship to MM III force-wide impact. S
or
TS-FRD
1.5.g (X2)
If impact is or is suspected to be Minuteman III force-wide, classify TOP SECRET-FRD and submit to OO-ALC/LM and HQ AFSPC/DOM for classification determination.
CHAFF SUBSYSTEM
Information Revealing |
Classification Reason Date |
Remarks |
|
1 | Chaff subsystems: | ||
a. Max quantity of clouds that can be loaded or deployed. | S 1.5.g (X2) |
||
b. Quantity of chaff dispensers on an operational missile | S 1.5.g (X2) |
||
c. Max quantity of chaff clouds per chaff dispenser. | S 1.5.g (X2) |
||
2 | Chaff dispensers: | ||
a. Chaff dispenser excluding boats | U |
||
b. Chaff boats excluding dipoles | S 1.5.g (X2) |
Visual and physical access | |
3 | Chaff attachment kit: | ||
a. Power distribution panel. | U to S 1.5.g (X2) |
Visual access UNCLASSIFIED
Physical access SECRET |
|
b. Converter (setting module). | U to S 1.5.g (X2) |
Visual access UNCLASSIFIED
Physical access SECRET |
|
c. Dispenser controller. | U to S 1.5.g (X2) |
Visual access UNCLASSIFIED
Physical access SECRET |
|
d. Hardness material | U to S 1.5.g (X2) |
Visual access UNCLASSIFIED
Physical access SECRET |
|
4 | Complete chaff subsystem (actual or engineering mockup): | ||
a. With carriers or dipoles | |||
|
S 1.5.g (X2) |
Visual and physical access | |
|
U to S 1.5.g (X2) |
Visual access UNCLASSIFIED
Physical access SECRET |
|
b. Without carriers or dipoles. | |||
c. Dipoles alone. | S 1.5.g (X2) |
Visual and physical access | |
5 | Chaff subsystem: | ||
a. Wire lengths | S 1.5.g (X2) |
||
b. Wire diameters | S 1.5.g (X2) |
||
c. Wire materials. | C 1.5.g (X2) |
||
d. Weight. | C 1.5.g (X2) |
||
6 | Broad Band Unit (BBU) radar cross section: | ||
|
S 1.5.g (X2) |
||
|
S DECLAS 1.5.g (X2) |
||
c. Operating characteristics | S 1.5.g (X2) |
||
d. Cloud geometry (length, width). | S 1.5.g (X2) |
||
e. Composition of BBU. | S 1.5.g (X2) |
||
7 | Physical unmasking altitude. | S 1.5.g (X2) |
|
8 | Doppler unmasking altitude. | S 1.5.g (X2) |
|
9 | Chaff survival altitude. | S 1.5.g (X2) |
|
10 | Chaff deployment parameters | ||
|
S 1.5.g (X2) |
||
|
S 1.5.g (X2) |
||
|
S 1.5.g (X2) |
||
|
S 1.5.g (X2) |
||
|
S 1.5.g (X2) |
||
f. Chaff ejection velocity. | S 1.5.g (X2) |
||
11 | Reliability. | S 1.5.g (X2) |
|
12 | Chaff test configuration designed for development tests, flight-proof tests and qualification tests | Classify per this Guide according to information revealed. | |
13 | Vulnerability to countermeasures | ||
a. Techniques for discrimination between the RV/decoy-bearing chaff cloud and non-RV/decoy- bearing chaff clouds. | TS or TS-FRD 1.5.g (X2) |
If vulnerability to countermeasures or a method of discrimination is revealed, HQ AFSPC/DO approval for release or dissemination is required. TOP SECRET-FRD if nuclear weapon information is revealed. See RV guides. | |
b. Ways of discriminating between decoys and RVs. | TS-FRD 1.5.g (X2) |
||
14 | Weight: | ||
a. Chaff dispenser including chaff | S 1.5.g (X2) |
||
b. Chaff dispenser excluding chaff. | U |
||
c. Chaff attachment kit. | U |
||
d. Weight of puff or BBU. | S 1.5.g (X2) |
||
15 | Fact that there is a chaff-masking design requirement. | U |
If design requirements are revealed, classify per this Guide, as appropriate. |
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PART C
DECOY SUBSYSTEM
Information Revealing |
Classification Reason Date |
Remarks |
|
1 | Decoy subsystem: | ||
a. The fact that the Pen Aid system can contain more than one decoy. | U |
||
b. Max quantity of decoys that can be loaded or deployed. | S-FRD 1.5.g (X2) |
Could reveal max RVs which could be loaded or deployed | |
2 | Decoy assembly: | S 1.5.g (X2) |
|
a. Nose. | U to S 1.5.g (X2) |
Visual access UNCLASSIFIED
Physical access SECRET |
|
b. Ballast. | U to S 1.5.g (X2) |
Visual access UNCLASSIFIED
Physical access SECRET |
|
c. Aft section. | U to S 1.5.g (X2) |
Visual access UNCLASSIFIED
Physical access SECRET |
|
d. RF Enhancer. | S 1.5.g (X2) |
||
e. Seeding ring. | U to S 1.5.g (X2) |
Visual access UNCLASSIFIED
Physical access SECRET |
|
3 | Decoy erection and ejection mechanism: | ||
a. Platforms. | S 1.5.g (X2) |
||
b. Ejection mechanism. | U |
||
4 | Complete decoy subsystem engineering mockup (including decoys and decoy platform kit). | S 1.5.g (X2) |
|
5 | Physical characteristics: | ||
a. External configuration. | S-FRD 1.5.g (X2) |
||
b. External dimensions | U |
||
c. Weight | S-FRD 1.5.g (X2) |
||
d. Center of gravity. | S-FRD 1.5.g (X2) |
||
e. Moments of inertia. | C-FRD 1.5.g (X2) |
||
f. Products of inertia. | U |
||
g. Ballistic coefficient. | S-FRD 1.5.g (X2) |
||
6 | Materials: | ||
a. Heat shield | U to TS-FRD 1.5.g (X2) |
If hardness information is revealed, then classify CONFIDENTIAL to TOP SECRET-FRD. See Section XIV. | |
b. Nose. | U to TS-FRD 1.5.g (X2) |
See para 6.a. above. | |
c. Structure. | U |
||
d. Enhancer | S-FRD 1.5.g (X2) |
||
e. Ballast plating. | S-FRD 1.5.g (X2) |
||
7 | Radar cross section | S to S-FRD 1.5.g (X2) |
Includes design requirements. SECRET-FRD if RV data is revealed |
8 | Aerodynamics performance. | S to S-FRD 1.5.g (X2) |
SECRET-FRD if RV performance revealed |
9 | Fluid dynamics performance | S-FRD 1.5.g (X2) |
Simulates RV performances. See RV guides. |
10 | Thermodynamics performance. | S-FRD 1.5.g (X2) |
Simulates RV performances. See RV guides. |
11 | Performance altitude | ||
a. Simulation of RV signature and trajectory. | S-FRD 1.5.g (X2) |
Simulates RV performances. See RV guides. | |
b. Survival. | S-FRD 1.5.g (X2) |
Simulates RV performances. See RV guides. | |
12 | Reliability. | S-FRD 1.5.g (X2) |
Simulates RV performances. See RV guides. |
13 | Decoy test configuration for: | ||
a. Radar range measurements | S-FRD 1.5.g (X2) |
Simulates RV performances. See RV guides. | |
b. Vacuum chamber, wind tunnel or arc jet tests. | S-FRD 1.5.g (X2) |
Simulates RV performances. See RV guides. | |
c. Flight-proof tests. | S-FRD 1.5.g (X2) |
Simulates RV performances. See RV guides. | |
d. Qualification tests. | S-FRD 1.5.g (X2) |
Simulates RV performances. See RV guides. | |
14 | Vulnerability to countermeasures. | S-FRD to TS-FRD 1.5.g (X2) |
Up to TOP SECRET-FRD if RV information is revealed. See RV guides. |
15 | Deployment parameters | ||
a. Decoy ejection velocity | S-FRD 1.5.g (X2) |
Simulates RV performances. See RV guides. | |
b. CEP | S-FRD 1.5.g (X2) |
Simulates RV performances. See RV guides. | |
c. Lateral separation accuracy. | S-FRD 1.5.g (X2) |
Simulates RV performances. See RV guides. | |
d. Spin rate. | S-FRD 1.5.g (X2) |
Simulates RV performances. See RV guides. | |
16 | Complete design, operating performance of the operational ejection mechanism. | Classify per this Guide according to information revealed. | |
17 | Weight: | ||
a. Decoy. | S 1.5.g (X2) |
||
b. Platform kit. | U |
||
c. Components. | U |
||
18 | Operational evaluations of decoy performance against design requirements. | S to TS-FRD 1.5.g (X2) |
Up to TOP SECRET-FRD if RV information is revealed. See RV guides. |
19 | Association of MM III Pen Aids with their mission. | S 1.5.g (X2) |
See paras 9 and 16 |
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SECTION XIX
SOFTWARE AND DATA
References:
a. CJCSI 3231.01, ÂSafeguarding the Single Integrated Operational Plan, dated 30 November 1993. Classified by: Director, J-3, Declassify on: 1.5.g (X2)
b. CG-W-5, Joint DOE/DoD Nuclear Weapon Classification Policy Guide, dated January 1994. Classified by: Robert T. Duff, J-3 Director, Office of Classification, Department of Energy.
c. Strategic Target Planning Security Classification Guide, dated 3 February 1997. Classified by: Vice Admiral Dennis A. Jones, Deputy Commander in Chief, United States Strategic Command . Reason: 1.5a. Declassify on: X4.
Information Revealing |
Classification Reason Date |
Remarks |
|
1 | ICBM target cases. | S-FRD or TS-FRD SIOP-ESI (Cat 06) 1.5.a |
Classified by references a, b, and c. Target cases for an entire unit (a missile squadronÂs on-alert sorties) are TOP SECRET-FRD/SIOP-ESI (Cat-06). |
2 | ICBM execution plan cases | S 1.5.a (X4) |
Classified by reference c. Execution plan cases do not reveal launch times, penetration times, or times on target. |
3 | ICBM target verification response delay times. | U |
Mark and protect as FOUO. |
4 | Execution plan program | U |
Two-person concept material. |
5 | MM Targeting Program: | ||
a. MM II: | |||
|
|||
|
S 1.5.g (X2) |
||
|
S 1.5.g (X2) |
||
|
U |
||
|
S 1.5.g (X2) |
EWO target tapes are two-person concept material. Special/Training target tapes are not two-person concept material. | |
|
S 1.5.g (X2) |
Handle as two-person concept material | |
b. MM III CDB: | |||
|
S-FRD 1.5.g (X2) |
Two-person concept material. Engineering version copies are not two-person concept material. | |
|
S 1.5.g (X2) |
Handle as two-person concept material | |
|
S-FRD 1.5.g (X2) |
Handle as two-person concept material | |
|
U |
Two-person concept material. | |
|
TS 1.5.g (X2) |
Handle as two-person concept material | |
c. HQ AFSPC production programs: | |||
|
S-FRD 1.5.g (X2) |
||
|
S-FRD 1.5.g (X2) |
Two-person concept material. | |
|
S-FRD 1.5.g (X2) |
Two-person concept material. | |
|
|||
|
U |
||
|
U |
||
|
S 1.5.g (X2) |
||
|
U |
||
6 | Program tapes: | ||
a. Program Tape, Fig A 13001 (Grd/FL WS-133B) | S 1.5.g (X2) |
Tape P/Ns 20032-309-11, -211 and -401 | |
b. Program Tape, Fig A 13001M (Grd/FL WS-133A-M) | C 1.5.g (X2) |
Tape P/N 20264-309-11 pre-ARSIP, ARSIP, P/Ns 20264-309-1 and -21 (SASS) | |
c. Fig A 13001M | C 1.5.g (X2) |
Tape P/N 20264-309-201 (ILCS) Flight Tape Only). Pre-ARSIP P/N 20264-309-31. | |
d. Wing Code Processing System Master Program Tape CI 0045871 | S 1.5.g (X2) |
Tape P/N 10803-309-41 (CCOS PROG EXE) | |
e. Operational Flight (IMU) Tape, Fig A 17913 and CI 19243. | S 1.5.g (X2) |
Tape P/Ns 20208-309-11 and 20346-309-1 | |
f. CMSC Program Tape, Fig A 13229 (WS-133B) | S 1.5.g (X2) |
Tape P/N 10061-309-11 | |
g. CMSC Program Tape, Fig A 13229M (WS-133A-M). | C U 1.5.g (X2) |
Tape P/N 10079-309-7 | |
h. Overwrite Program Tape, CI 19230. | C 1.5.g (X2) |
Tape information content is UNCLASSIFIED. Access is CONFIDENTIAL to preclude unauthorized access and tampering due to potential to cause incomplete overwrite. Tape P/N 20364-309-11. | |
i. Certification Program, Fig A 17841. | C 1.5.g (X2) |
Tape P/N 10394-309-1 and -11 | |
|
S DECLAS 31 DEC 2007 |
WS-133A-M, Tape P/N 20149-309-1, -11 (Basic); 20343-309-201, -301, -1, -11 (CDB); 20382-309-1, -11, -21 (HEG). WS-133B Tape P/N 20151-309-1, -11 (Basic); 20370-309-1 (CBD), -11 (HEG) | |
k. Program Tape Fig A 14250 | U |
||
l. MAF Encryption Program Tape (SSAS) | S 1.5.g (X2) |
Controlled COMSEC Item. Tape P/N 25-76579-1. | |
m. LF Encryption Program Tape (SSAS), USKAF-9, Fig A 17797. | S 1.5.g (X2) |
Controlled COMSEC Item. Tape P/N 20268-309-1. | |
n. Overwrite Program Fig A 13231 (ILCS Configuration) | C 1.5.g (X2) |
Tape information content is UNCLASSIFIED. Access is CONFIDENTIAL to preclude unauthorized access and possible tampering due to potential to cause incomplete overwrite. Tape P/Ns 20294-309-1, -11, and -21. | |
o. Operational Ground Program Tape, CI 19236 (ILCS) Configuration) - pre-ARSIP. ARSIP CI 19236AA | U |
ARSIP Tape P/Ns 20283-309-1, -11, -21, and -31 | |
p. Assembly and Checkout Program Tape, CI 19237 (ILCS Configuration). | U |
Tape P/N 20286-309-1 | |
q. Operational Ground Program Tape, CI 19240 (WS-133A-M) - pre-EEP EEP CI 19240AA. | C U 1.5.g (X2) |
Tape P/Ns 20277-309-1 (GIP) and -11 (MESP) and -21 (EEP) | |
r. Operational Ground Program Tape CI 19241 (WS-133B)-Pre-EEP EEP CI 19241AA | C 1.5.g (X2) |
Tape P/N 20280-309-1 (GIP) and -11 (MESP) and -21 (EEP) | |
s. Operational Flight Program (OFP) Tape, CI 19220 | S 1.5.g (X2) |
Tape P/Ns 20376-309-1 and -11 | |
t. MM III OFP Tape CI 19243. | S 1.5.g (X2) |
Tape P/N 20289-309-1 | |
u. Operational Ground Program Tape, CI 19244 (ERCS/ILCS). | U |
Tape P/N 20241-309-1. | |
|
S 1.5.g (X2) |
Tape P/Ns 20099-309-5 and 20274-309-1, -201, and -211 | |
|
S 1.5.g (X2) |
Tape P/Ns 20379-309-1 (OP) and -201 (OTL) (MK12); 20292-309-1 and 201 (MK12A); 20379-309-11 and 211 (SRV); 20292-309-11 and 211 (SRV). | |
|
U |
Tape P/N 10806-309-41 | |
y. MM Application Program CI 0045874. | U |
Tape P/N 10812-309-61 | |
z. MMIII GRP Operational Ground Program WS-133AM, WS-133B CI S-133-19251 | U |
No separate tape. GRP OGP combined both AM and B system programs into a single program that supports both configurations. CPIN No. 82A-NS50/LGM30G-F001-00D. | |
aa. MMIII GRP Operational Flight Program WS-133AM, WS-133B CI S-133-19252. | U |
No separate tape. CPIN No. 82A-NS50/ LGM30G-F002-00D. | |
ab. MMIII GRP Operational Ground Flight Program CI S-133-19250 | U |
Tape P/N 20426-309-(). OGP/OFP combined for both AM and B Systems. | |
ac. MMII GRP MK12A Flight Program Constants Tapes CI S-133-19253. | S 1.5.g (X2) |
Tape P/N 20429-309-() (Type I), DC300 cartridge magnetic tape for the
Operational Program. Tape P/N 20429-309-() (Type 2) DC300 cartridge
magnetic tape for the Operational Training Launch program at VAFB. CPIN No. 82A-NS50/MK12A/F001-00A (Operational) CPIN No. 82A-NS50/MK12A/F002-00A (Operational Training Launch) |
|
ad. MMIII GRP MK12 Flight Program Constants Tapes CI S-133-19254 | S 1.5.g (X2) |
Tape P/N 20433-309-() (Type 1) DC300 cartridge magnetic tape for the
Operational program. Tape P/N 20433-309-() (Type 2) DC 300 cartridge
magnetic tape for the Operational Training Launch program at VAFB. CPIN No. 82A-NS50/MK12/F001-00A (Operational). CPIN No. 82A-NS50/MK12/F002-00A (Operational Training Launch |
|
7. | Execution/Targeting Software and Databases | ||
a. Console Operations Program (COP EXE) CSCI 0036000 | U |
WSP main program - provides command, control, communication. P/N C006839-02 | |
b. COP Database, CSCI 0036000 | U |
COP screen templates, etc. P/N C006839-03 | |
c. COP User ROM (Firmware), CSCI 00360; COP FDM Format CSCI 0036000 | U |
WSP firmware. P/Ns C006839-04 and C006839-05, respectively. Included in initial Computer Memory Security (CMSC). | |
d. COP Boot ROM, CSCI 0036000 | U |
WSP boot firmware, P/N C006839-06. Included in initial CMSC. | |
e. Execution Plan Program (EPP) Exe. CSCI 19291 | U |
Provides execution plan processing. P/N 103-1929111-01 | |
f. MOTP3 Exe. CSCI 19215 | S-FRD 1.5.g (X2) |
The MOTP3 provides targeting processing | |
g. Trajectory and Missile Parameters (TAMP) | S-FRD 1.5.g (X2) |
The TAMP provides trajectory and missile parameters | |
h. Operational Ground Program Offload Tape | U |
Loaded to the WSCE for transfer to the LF. Executable in the MM flight computer, not in the console | |
i. EPP/Message Analysis (MA) Databases (DBs) | TS-FRD SIOP-ESI Cat 10 1.5.g (X2)
|
The EPP portion provides the execution plan database (DB) for the EPP and COP. The MA portion provides the database for the COP. TOP SECRET for training values, TOP SECRET SIOP-ESI for actual values as provided by OL-B, HQ AFSPC/DO. | |
j. MOTP3 DB | S-FRD 1.5.g (X2) |
Targeting database for the MOTP3. | |
k. Force Direction Message (FDM) Format DB | U |
Format database for force direction messages. | |
l. TCI/EPCI DB (Also Case Image Data) | S to TS-FRD SIOP-ESI Cat 6 and 10 1.5.g (X2) |
Target cases provide case input data for targeting and execution plans. Classification is dependent upon targeting data and number of sorties as provided by OL-B, 625 MOF/TAB. For upload via Floppy diskette, diskette retain original classification if write-protect tab is set during upload. | |
m. Tech Order DB | U to TS-FRD SIOP-ESI Cat 6 and 10 1.5.g (X2) |
Technical order database uploaded to COP via Floppy disk. Floppy diskette remains UNCLASSIFIED if write-protect tab is set during upload, otherwise diskette assumes the highest classification of information in the system. | |
n. Transmission Integrator (TI) CSCI 00500 | U |
Prepares messages for transmission over different HA communications systems. | |
o. Communications Integrator/Backup (CI/CIB) CSCI 00400 | U |
Prepares messages received over different HA communications systems for processing by the MP. As backup, transfers incoming message text to WSCE for printing. | |
p. Message Processor (MP) CSCI 00300 | TS-SIOP-ESI, Cat 6 and 10 1.5.g (X2) |
Performs rapid message processing functions | |
q. Code Change Upload Floppy diskette (CMSC Control words) | U |
Floppy disk is generated at the WCPS for upload at the LCC, NSA supplied control words for the computer memory security check are encrypted. Floppy diskette remains Unclassified if write-protect tab is set during upload. | |
8 | Trainer Software | ||
a. Operations Trainer Software | |||
|
U |
PDP-11/34 operating system. Resident on diskpack. | |
|
U or S 1.5.g (X2) |
Simulates AFSATCOM, SLFCS, and SACDIN communications system functions, Also used to generate and execute instructor messages and system parameters that can be classified SECRET. UNCLASSIFIED or SECRET depending on level of information loaded. Resident on diskpack | |
|
U or S 1.5.g (X2) |
Comprised of instructor databases that are either UNCLASSIFIED or SECRET. Resident on diskpack. | |
|
U or S 1.5.g (X2) |
Simulates operational status and command systems. Operates on the MPC-1624 computer. Basic software is UNCLASSIFIED however it is used to generate and execute lesson plans that can be classified SECRET. UNCLASSIFIED or SECRET depending on the level of information loaded. Resident on floppy diskettes. | |
|
U or TS 1.5.g (X2) |
Operates on the MPC 1624 computer. Basic software is UNCLASSIFIED however it is used to generate instructor databases that can be classified TOP SECRET. Resident on floppy diskettes. | |
|
U or TS 1.5.g (X2) |
Comprised of instructor databases that are UNCLASSIFIED, SECRET, or TOP SECRET. Resident on floppy diskettes. | |
|
U |
VAX-11/750 and 751 operating system. Resident on diskpack. | |
|
U to TS 1.5.g (X2) |
Simulates operational status and command systems. Operates on VAX-11/751 computer. Basic software is UNCLASSIFIED however it is used to generate and execute lesson plans that can be classified SECRET and execution data that can be TOP SECRET. Resident on disk pack. | |
|
U |
Instructor terminals operating system. | |
|
U to TS 1.5.g (X2) |
Comprised of instructor databases that are either UNCLASSIFIED, SECRET or TOP SECRET. Resident of floppy diskettes. | |
|
U to TS 1.5.g (X2) |
Simulates operational status and command systems. Operates on VAX-11/750 computer. Basic software is UNCLASSIFIED however it is used to generate and execute lesson plans that can be classified SECRET and execution data that can be TOP SECRET. Resident on diskpack. | |
|
U to TS 1.5.g (X2) |
Comprised of instructor data bases that are either UNCLASSIFIED, SECRET or TOP SECRET. Resident on diskpack. | |
b Procedures Trainer Software | |||
|
U |
Used in the AM System RY MPT and MEPT. Resident on RSE. | |
|
U |
Used in the B System LE MPT and MEPT. Resident on RSE. | |
|
TS 1.5.g (X2) |
Used in the AM System RY MPT, B System LE MPT and MEPT. Same as operational EPP/MA database, except contains training values. Part of MPTCP program - resident on RSE. | |
|
TS 1.5.g (X2) |
Used in the AM System RY MPT, B System LE MPT and MEPT. | |
|
U to TS 1.5.g (X2) |
Used in the AM System RY MPT B System LE MPT. Classified upon use. | |
|
U |
VAX operating system resident on RSE. | |
|
U |
Audio controller computer operating system resident on RSE and downloaded to audio buffer. Also on floppy diskettes. | |
|
U |
Resident on RSE. | |
|
U |
Resident on RSE and on tape. | |
|
U to TS 1.5.g (X2) |
|
|
|
U |
Data generated to test the floppy disk drive. Resident on diskette |
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SECTION XX
RAPID MESSAGE PROCESSING
Information Revealing |
Classification Reason Date |
Remarks |
|
1 |
|
||
|
U |
||
|
U |
||
|
TS 1.5.g (X2) |
||
|
UNCLASSIFIED unless classified according to the information contained therein. All copies shall be protected against modification or substitution at the TOP SECRET level and shall be marked ìCONTROLLED AS TOP SECRET FOR PROTECTION AGAINST UNAUTHORIZED MODIFICATION.î | ||
e. Threats identified against communication channels. | S 1.5.g (X2) |
||
2 |
|
||
a. A list of higher authority communication equipment connected to RMP. | U |
||
b. A partial list which identifies some communication systems over which EAMs are transmitted. | U |
||
c. A complete list or compilation of partial lists which identifies all communication systems over which EAMs are transmitted. | S 1.5.g (X2) |
||
d. A partial list which associates specific JCS and USSTRATCOM messages with specific communication systems. | S 1.5.g (X2) |
||
e. A complete list or compilation of partial lists which associates all JCS and USSTRATCOM messages with all communication systems over which they will be transmitted. | TS 1.5.g (X2) |
||
f. Processor sizing, power requirements for system components. | U |
||
3 | Messages: | ||
a. The fact that EAMs direct the war and may generally contain or be used to determine necessary data such as authentication codes, time values, and targeting support information. | U |
||
b. A partial list or catalog of messages and types. | S 1.5.g (X2) |
||
c. A complete list or catalog of messages and types which does not include countries, targets, or execution or termination values | S 1.5.g (X2) |
||
d. Information which reveals the detailed format, range of values, or function of specific EAMs. | S to TS 1.5.g (X2) |
||
e. Maximum message length that RMP can accommodate. | U |
||
f. Bit-level message characteristics and wave-forms, character coding schemes such as PLSO and STUTTER. | U |
||
4 |
|
||
|
U |
||
|
S 1.5.2 (X2) |
||
c. Piecing, the term itself. | U |
||
d. Any media (document, software, firmware, hardware) which reveals JCS prescribed message piecing processes. | S 1.5.g (X2) |
||
e. Message throughput rates and false message rates. | S 1.5.g (X2) |
||
f. Overall processing time. | U |
||
g. Data base organization and format. | Dependent upon the classification of the data revealed. | ||
h. Source code, object code. | Dependent upon the classification of the data revealed. | ||
5 | Complete or end items: | ||
a. System limitations. | S 1.5.g (X2) |
||
b. Complete set of drawings or photographs. | U |
||
c. Complete/detailed system description or requirements | S 1.5.g (X2) |
||
6 |
|
||
|
S 1.5.g (X2) |
||
|
S 1.5.g (X2) |
||
|
U |
||
|
U |
||
|
S 1.5.g (X2) |
||
|
U |
||
g. Operations performed on codebooks (e.g., superseding of editions). | U |
||
h. NSA provided sample operational codebook material (over the air). | S-CRYPTO 1.5.g (X2) |
||
i. NSA provided sample operational codebook material (not over the air). COMSEC Controlled Item. | S 1.5.g (X2) |
||
j. Maximum sizes, page-counts, parts, fields, or systems. | U |
||
7 |
|
||
a. Overall processing time for EAMs. | U |
||
b. Specific processing for each message. | S 1.5.g (X2) |
||
8 | Database values: | ||
a. Specific operational or high fidelity test database value: | Non-specific databases for test purposes may range from UNCLASSIFIED to TOP SECRET. AFSPC hardware and software must be able to handle and process operational databases classified as TOP SECRET/SIOP ESI/CRYPTO. | ||
|
TS-SIOP- ESI 1.5.g (X2) |
||
|
S-CRYPTO 1.5.g (X2) |
||
|
TS/SIOP- ESI 1.5.g (X2) |
||
|
S 1.5.g (X2) |
|
MEMORANDUM FOR DISTRIBUTION
FROM: OO-ALC/CC
7981 Georgia St.
Hill AFB, UT 84056-5824
SUBJECT: Change 1, ICBM Security Classification Guide (SCG), 30 Sep
97
1. The changes which comprise change 1 to the current ICBM SCG are identified below. They should be posted in the SCG and this letter retained in the SCG.
(a) Attachment 1, page 34, paragraph 3.e.(2) to read:
Number of RVs on an operational S-FRD See 3.e.(5)
missile in any given
LF
1.5.g (X2)
(b) Attachment 1, page 34, add sub-paragraph 3.e.(5)
For the 90th Space Wing only, U START 1 compliance
the fact that any LF has only
one RV, or that it is SRV.
(c) Attachment 1, page, 50, paragraph 1.h.(3).(f).(6) to read:
Test Launch site coordinates U or C UNCLASSIFIED when World
1.5.g (X2) Geodetic System (WGS)
coordinates for the LF are not
provided. CONFIDENTIAL
when WGS coordinates are
provided.
(d) Attachment 1, page 50, paragraph 1.k.(1) to read:
If launch site WGS coordinates
included
C
See Section XIII.
(e) Attachment 1, page 60, paragraph 7.a.(1) to read:
WGS coordinates (>, S) U or C UNCLASSIFIED when given
1.5.g (X2) no more precisely than the
closest minute.
(f) Section V, Distribution, page 19 to read:
HQ USSTRATCOM
J005, Ste 1H9, -6005
J312/331/334/362/441/443, Ste BA3, -6300
J511/ 523/541, Ste 2E8, -6500
J613, Ste 2B9, -6600
901 SAC Blvd
Offutt AFB NE 68113-xxxx
(g) Section V, Distribution, page 18 to read:
HQ AFSPC/
DOM -4180
DOTO -4240
DRM -4670
LGM -4470
SCOMG -4400
SEWM -4260
SFPON -4560
150 Vandenberg St, Ste 1105
Peterson AFB, CO 80914-xxxx
(h) Section V, Distribution, page 13 to read:
791 MXS/CC
319 SPS/SPAI
MAIL ALL COPIES TO
450 G St, STE 321
Grand Forks AFB, ND 58205-6023
341 LG/CC
LSS/CC
MXS/CC
OG/CC
43 SPS/SPAII
MAIL ALL COPIES TO
341 LG, BLDG 500, STE 148, 2177 St N.
Malmstrom AFB, MT
59402-7538
(i) Section V, Distribution, page 14 to read:
90 LG/CC
LSS/CC
MXS/CC
SSS/SPAI
MAIL ALL COPIES TO
5305 Randall Ave
Francis E Warren AFB, WY 82005-2274
91 LG/CC
LSS/CC
MXS/CC
OS
5 SPS/SPAI
MAIL ALL COPIES TO
5 MSS/MSIAC, 220 Peacekeeper PL
Minot AFB, ND 58705-5000
(j) Section V, Distribution, pages 16 and 17 delete the
following:
ÂDefenseTechnical Information Center  and ÂDTICÂ
Cameron Station
Alexandria, VA 22304-6100/-6145
(k) Section V, Distribution, page 16 add:
 Defense Logistics Agency
8725 John J Kingman Road
STE 2533
Fort Belvoir, VA 22060-6221Â
(l) Section V, Distribution, page 14 to read:
Change AFLC to AFMC
Wright Patterson AFB, OH 45433-5260
MME
SFX
SCWM
(m) Section V, Distribution, page 20 change as follows:
Under OO-ALC change 75 SFS/SFAI
TO 75 SFS/SFA
(n) Section V, Distribution, page 15 change Capital Hill Area, DIS location
Alexandria to;
Greater Baltimore/Washington, D.C.
Defense Security Service Location
Hoffman Building
2461 Eisenhower Avenue, Room 744
Alexandria, VA 22331-1000
(o) Section V, Distribution, page 15 change Central Region, DIS location
Chicago to:
Midwest
Defense Security Service Location
610 South Canal Street, Room 800
Chicago, IL 60607-4599
(p) Section V, Distribution, page 15 change Central Region, DIS location
Irving to:
Texas/Oklahoma
Defense Security Service Location
5800 E. Campus Circle Drive
Suite 110A
Irving, TX 75063-2739
(q) Section V, Distribution, page 20 change Northeast Region, DIS location to:
Mid-Atlantic
Defense Security Service Location
770 Wood Lane
Suite 12
Mt. Holly, NJ 08060-3802
(r) Section V, Distribution, page 21 change Pacific Region, DIS location
to:
Southern California
Defense Security Service Location
One World Trade Center
Suite 622
Long Beach, CA 90831-0622
(s) Section V, Distribution, page 22 change Southeastern Region, DIS
location to:
Gulf Coast
Defense Security Service Location
2300 Lake Park Drive
Suite 250
Smyrna, GA 30080
2. Point of contact is Mr. Milton Johnson, LMEA, DSN 777-7799, FAX
777-4643.
ORIGINATING
OFFICIAL:
COORDINATING OFFICIAL:
CARL B. OVERALL, Col, USAF TIMOTHY G. HARDY, Lt Col, USAF
Program Director Commander, 75th Security Forces Squadron
ICBM System Program Office
APPROVING OFFICIAL:
RICHARD H. ROELLIG, Major General, USAF
Commander
|
DEPARTMENT OF THE AIR FORCE
HEADQUARTERS OGDEN AIR LOGISTICS CENTER (AFMC)
HILL AIR FORCE BASE, UTAH
25 Jan 2001
MEMORANDUM FOR DISTRIBUTION
FROM: OO-ALC/LM
6014 Dogwood Avenue
Hill AFB UT 84056-5816
SUBJECT: Change 2, ICBM Security Classification Guide (SCG), 30 Sep
97
1. The changes which comprise change 2 to the current ICBM SCG are identified
below. They should be posted in the SCG and this letter retained in the
SCG.
(a) Section IV, page 11, add a new paragraph ac: SERV. Safety Enhanced Reentry Vehicle.
Renumber remaining paragraphs accordingly.
(b) Section V, Distribution, page
14 add:
90 OG/CC
91 OG/CC
(c) Attachment 1, Section XIV,
page 67, paragraph c change XOFS to XONO.
(d) Attachment 2, Section X, page
31, paragraph c change XOFS to XONO.
(e) Section V, Distribution, page
14 add:
HQ AFDO/CC
1720 Air Force Pentagon
Washington DC 20330-1720
HQ AFHRA/RSA
600 Chennault Circle
Maxwell AFB AL 36112
(f) Section V, Distribution, page
16 add:
Defense Technical Information Center
8725 John J. Kingman Road, Suite 944
Fort Belvoir VA 22060-6218
(g) Section V, Distribution, pages
15, 20, 21, and 22 delete the following:
AFWL/SP and all DSS locations
(h) Section V, Distribution, page
14 delete the following:
AFSAA/SAI
(i) Section V, Distribution, page
14 to read:
HQ AFMC/SFXP
Bldg 266, Rm N208
4225 Logistics Ave
Wright Patterson AFB OH 45433-5760
HQ AFMC/XRS, STE 6
4315 Chidlaw Rd
Wright Patterson AFB OH 45433-5006
ASC/SP, Rm 103A
1801 10th ST
Wright Patterson AFB OH 45433-6825
FASTC/SP, STE 1, Bldg 11A, Rm 013
1970 3rd St
Wright Patterson AFB OH 45433-6504
HQ USAF/XOFI
1340 Air Force Pentagon
Washington DC 20330-1340
(j) Section V, Distribution, page
22, change as follows:
Was:
TRW Strategic Systems Division
Systems Integration Group
1104 Country Hills Drive
Ogden UT 84403-2400
Is:
TRW ICBM Systems
ATTN: Security
P.O. Box 804
Clearfield UT 84089-0804
(k) Add attachment 1 to appropriate
sections of the SCG as noted.
(l) Add attachment 2 to appropriate
section of the SCG.
2. The above changes consist of revising the IMPSS security and Hardware
Classification sections and updating the distribution list. The information
contained herein is not to be released on the Internet.
3. Point of contact is Mr. Milton Johnson, LMEI, DSN 777-6933, FAX
777-4643.
COORDINATING OFFICIAL: ORIGINATING OFFICIAL:
WARREN L. KEITHLEY, Major, USAF CARL B. OVERALL, Colonel, USAF
Commander, 75th Security Forces Squadron Program Director
ICBM System Program Office
Attachments:
1. ICBM Security Classification Guide Weapon System Security Section
2. ICBM Security Classification Guide Attachment 1 (Minuteman), Section
II
APPROVING OFFICIAL:
SCOTT C. BERGREN, Major General, USAF
Commander, Ogden Air Logistics Center