(UNTITLED)

• Document Type: CREST
• Collection: General CIA Records
• Document Number (FOIA) /ESDN (CREST): CIA-RDP79R00961A000400020008-4
• Release Decision: RIPPUB
• Original Classification: K
• Document Page Count: 11
• Document Creation Date: December 12, 2016
• Document Release Date: March 5, 2002
• Sequence Number: 8
• Content Type: HW

Approved For Release 2002/05/20 : CIA-RDP79R00961A000400020008-4
25X1
Approved For Release 2002/05/20 : CIA-RDP79R00961A000400020008-4
 SECRET
THIS IS A COVER SHEET
The information in this document
is classified and as such will be
treated according to OSD Security
Instructions. Writing on this
cover sheet is prohibited.
SECRET
 Approved For R ease 0069a: CIA-RDP79ROO
S.F-CRET/NOF RN
SPECIFIC INTELLIGENCE COLLECTION REQUIREMENT
2. TO
3. EXPIRATION DATE
12 October 1962
4. CONTROL NUMBER
D-ACQ-02801
5. DISPATCH DATE
6. PRIORITY
1C
7. SUBJECT
S. COUNTRY
U) Anti-Ballistic Missile Systems 7
USSR
Items to be enteeed in this space will be as follows (In the sequence indicated); 0. REQUIREMENTS; 10. BACKGROUND; 11. GUIDANCE;
12
A
.
TTACHMENTS
9. (SECRET/NOFORN) REQUIREMENTS:
Information on possible Soviet anti-ballistic missile or anti-satellite systems
is needed to permit detailed analysis and determination of the following:
a. Overall system:
(1) Acquisition and tracking ranges, with a data tolerance of +
(2) Intercept altitude and range parameters, with a data tolerance of + 10%o.
(3) Minimum tracking time required, with a data tolerance of + 1 second.
(/k) Engagement sequence and problem solution times, with a data tolerance
of + 1 second.
(5) Component equipment tie-up time, i.e., time required before equipment
can be used for engagement of another target, with a data tolerance of + 1 second.
(6) Degradation of system capabilities for initial salvo and after each
successive salvo.
(7) Exact number of missiles which can be launched from each pad in a
given period of time; exact reload capabilities in a given period of time.
(8) Over-all system reliability, with a data tolerance of + 5%.
(9) Exact number of missiles required for a kill probability of one, two
and three sigma.
(10) Exact degree of system mobility.
EXCLUDED FROM AUTOMATIC REGRADING; DOD DIR 5200.10 DOES NOT APPLY
13. PORTIONS OF REQUIREMENT (Item
ASSIGNED TO ADDRESSEE FOR ACTION
14.
16. APPROVED FOR COLLECTION
` A f- T
a^
DD 1 FOR 621365
16. CLASSIFICATION
SECRET/NOFORN
6? A 002d0Q8t4 a
REPLACES ACSI FORM 1, 17 MAY 80,
OPNAV FORM 8820.6, OCT 58, AF
FORM 406, FES 61, WHICH MAY BE
USED UNTIL i JUNE 1962.
TELEPHONE NUMBER AND DATE
`4ajor J. A. Smith
'Q-1PD1 X 76845
'er 1 62
AGENCY APPROVAL
Jim
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 Approved For Release 2002/0 2QA cL RDP79R00961A000400020008-4
(11) Exact information on multiple target engagement capabilities
and maximum number which can be engaged simultaneously.
(12) Exact number of interceptor missiles which can engage a single
target.
(13) Exact entenk of system dead zones (missile, electronics, terrain).
(i1-) Site layout :
(a) Control points.
(b) Power supply.
(c) Fueling facilities.
(d) Location and size of missile handling equipment.
(e) Missile storage sites.
(f) Method of on-site transportation.
(g) Location of electronic items.
(h) Construction materials used.
(15) Specific locations of launch sites, support facilities and electronic
facilities; local ground environment; number and dimensions of revetments;
security.
b. Missiles:
(1) External configuration and dimensions, including weights, with a
data tolerance of + 1C%.
(2) Range and altitude parameters, with a data tolerance of + 1C%.
(3) Trajectories of R&D and training target missiles.
() Speed and maneuverability parameters, with a data tolerance of
kA F T_
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SECRET/NOFORN
SECRET/NOfORN
 cc T/NOFORN
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(5) Warhead subsystem:
(a) Type (HE or nuclear).
(b) Configuration.
(c) Weight.
(d) Yield, with a data tolerance of + 1 KT.
(e) Kill radii, with a data tolerance of + 100 ft.
(f) Fuzing.
(6) Guidance subsystem:
(a) Type (coi land, terminal homing)
(b) Accuracy (CEP, reliability) with a data tolerance of + 10 ft.
or +
(c) Vulnerability
(7) Propulsion subsystem:
(a) Type (liquid, solid, hybrid)
(b) Propellants.
(c) Propellant weight, with a data tolerance of + 10%.
(d) Engine/nozzle configuration.
c. Radar:
(1) Numbers
(2) Type (pulse or CW).
(3) Frequency, with a data tolerance of + 5 me up to 1000 me and _t 10 me
from 1000 me up.
(1k) Physical configuration and dimensions (photos or sketches are
desired):
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(a) Set proper.
(b) Antenna (including orientation and movement limitations).
(c) Other components (IFF, etc.),
(5) ECCM capabilities.
(6) Peak and average powers, with a data tolerance of + 10 KW average.
(7) Effective range and altitude capability5with a data tolerance of
(8) Discrimination capability.
(9) Vulnerability to countermeasures.
(10) MTI capability
(11) Scan rate, with a data tolerance of + 1O%~o.
(12) Tracking accuracy, with a data tolerance of + 10-20 ft.
(13) Azimuth and elevation limitations, with a data tolerance of + .5 deg.
(14+) Function or purpose of radar within target detection and/or missile
guidance system.
(15) Any functions other than missile defense.
d. Launcher:
(1) Configuration
(2) Exact number-of missiles for each unit.
(3) Azimuth and elevation limitations, with a data tolerance of +
(4) Firing positions, with a data tolerance of + 10.
(5) Slew rate, with a data tolerance of + 2?/sec.
(6) Vulnerability to attack or sabotage.
1) iz- A F- 7-
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e. Coirnnunications:
(1) Types.,
(2) Geographical location and directional orientation of communications
antennas.
(3) Number and type of buildings used in conjunction with communications.
f. Computers:
Time delay in computing and relaying information.
Physical size.
Power requirements.
How inputs and outputs are relayed.
g. Other ground handling equipment:
(1) Reload device
(a) Configuration
1 Track, trailer, other.
2 Railway sled, ram, other.
(b) Rates of movement, with a data tolerance of + 2-5 ft/sec or
+ 2 deg/sec.
(c) Capacity of movements
1 Exact number of missiles per unit.
2 Exact total number of missiles per unit.
(d) Location relative to launcher,
(2) Ready storage facility/equipment:
(a) Configuration.
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of + 25-30 ft.
(b)
Location with respect to launchers, with a data tolerance
(c)
(d)
(e)
Exact total capacity.
Rate of processing to reload device, with a data tolerance of
Functions served:
1 Strictly standby/hold area.
2 Missile subsystem check out
(f)
a Go/no go type.
b Detailed checkout type.
Vulnerability to attack or sabotage.
(3) Propellant handling equipment.
(4) Type and size of vehicles used with system, with particular emphasis
on resemblance to vehicles used with other systems such as SA-1 and SA-2.
h. Production facilities:
(1) Plants producing ABM systems or components.
(2) Design and production bureaus associated with ABM systems/components.
(3) Resources required to manufacture the various components.
(4) Rate of manufacture, with a data tolerance of 2-5 units/month.
i. Organizations, locations and personalities
(1) R&D organization and personnel for ABM development.
(2) Organization for inter-range coordination.
(3) Organization for deployment of ABM systems.
_ A F '
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10. (SECRET/NOF0RN) BACKGROUND:
a. Three complexes of unusual configuration have been reported under
construction and nearing completion in the Leningrad area, one approximately
30 KM NE of the city (30?44'W/60?05'N), one 65 KM NW (29044'W/60o26'N), and the
third 6o KM SW (29014'W/'59044,N).
b. Each of the complexes consists of a cluster of five launch sites. Each
site resembles an bperational SA-2 site with six launching pads forming a
circular arrangement. A circular access road forms the periphery around the site,
and in the center is Located what is most likely the control building (see
Attachments 1 & 2).
c. In addition to the suspected ABM complexes, the Soviets are suspected of
converting existing SA-1 and/or SA-2 sites to ABM sites. Sites C-05, c-16, C-~1.8,
in fe llMoSCo,,o aye&
C-31, E-19, E-23, E-24 and E-33Aare possibly being converted.
d. other possible areas where sites
are not limited to:
may be expected to appear include,
BAKU
KIYOV
ROSTOV
BRATSK
KOMSCMOL SK
SARY SHAGAN
CHITA
KUYBYSHOV
Sag PAL_A.TINSK
FERGANA
MINSK
STARAYA RUSSA
GORKIY
MOSKVA
SVERDLOVSK
KAMCHATKA
NOVOSIBIRSK
TASHKENT
KAZAN
ODESSA
TBILI SI
KHABAROVSK
RIGA
VLADIVOSTOK
KEIARKOV
1 A. FY
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e. A Soviet Bloc news release indicates that three radars are needed "to
guide and aim the anti-rockets". It has been estimated that a similar number
are needed in the ABM program, possibly:
(1) HEN ROOST for early warning
(2) FIRE WHEEL/SHIP 14TMEEL for interceptor tracking.
(3) HEN NEST/HEN EGG for tracking
A fourth radar, possibly a track-while-scan or a monopulse-type, may be used
for final tracking.
f. Since HEN ROOST is an extremely large installation, it may be easily
seen and recognized if the opportunity for observation arises. The launch
facilities, on the other hand, may be below ground and not readily apparent. For
this reason, radar siting will probably afford the best site signature for the
ABM system (see Attachments 4-6).
11. (CONFIDENTIAL) GUIDANCE:
a. The data tolerances listed in para 9 are the ultimate desired for analysis.
While every effort should be made to satisfy these tolerances in the collection
of intelligence, less accurate data will be useful in closing intelligence gaps.
b. AFM 200-14+, Chapter 13, contains intelligence collection guidance for
anti-ballistic missiles for defense systems. DIAv! 58-15, section two, provides
identification guidance of electronic systems.
c. This S1CR supersedes SiCR D-CIC-001+02.
S)(MC> Fort rii)
12., ATTACHMENTS:
a. Attachment 1 - SA-2 "Daisy-Link" Site and Individual ABM Launch Area.
b. Attachment 2 - Leningrad ABM Launch Complexes.
-RFA ~
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C.
Attachment 3
- Synthesized AM-1 Missile.
d.
Attachment 4
- Missile Beacon Tracking Radar.
e.
Attachment 5
- HEN NEST Radar.
f.
Attachment 6 - HE`N ROOST Radar.
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