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/specialCollection/MissileGap/1961/1961-04-25.pdf

Central Intelligence Agency · 101 pages · text from the file's own layer

This is National Intelligence Estimate 11-5-61, Soviet Technical Capabilities in Guided Missiles and Space Vehicles. It was submitted by the Director of Central Intelligence and concurred in by the United States Intelligence Board on 25 April 1961. The estimate assesses Soviet surface-to-air, antimissile, air-to-air, air-to-surface, ballistic, ICBM, naval and space programs. It concludes that the first Soviet ICBM unit was probably operational around 1 January 1960. It also says there is no evidence the Soviets are developing offensive space weapons. It contains no UFO material.

  • p. 15 …At the test range, the Soviets have fol- lowed a generally similar pattern in the de…
  • p. 33 …We believe that at the present time, the Soviets are well advanced in a program to…
  • p. 57 …the Soviet state of the art in re-entry techniques at that time. Subsequent advances in…
  • p. 58 …specific time designated well in advance, i.e., maximum readiness. The ready missile rate is expected…
  • p. 66 …program for developing advanced ASW weap- ons systems exists. The USSR has the basic scientific and…
  • p. 80 …technological advances in sev- eral key areas. 163.The Soviets are aware of the advantages offered…
  • p. 81 …The caliber of the Soviet work to date indicates that the USSR is among world leaders…
  • p. 82 …the vehicle should permit the Soviets to effect rendezvous with an earth orbiting vehicle. 173.Advanced…
  • p. 91 …We estimate the SS-6, and probably the SS-5, will probably utilize fixed sites. The…
  • p. 93 …The Academy of Sciences provides supplementary proposals and re- search programs designed to advance the state…
Table 2 (Continued)
SPUTNIK VII
(1981 BETA)
SPUTNIK VIII
(1001 GAMMA) Venus
Probe Success
SPUTNIK IX
(1081 THETA)
SPUTNIK N
(1061 IOTA)
SPUTNIK XI
(1961 MU)
Weight (lbs.)
Configuration
Diameter ((t) of SLIM-
Iltes.
Length (ft) of Sat,ellite
Date Launched
Orbit Period
Perigee (s.' m.)
Apogee (s. m.) ...L.
Inclination to Equator
(degrees).
Remarks
14,202
Unknown
Unknown
Unknown
4 Feb. 1001
80.8 up to Orbit
17 ..
135
194
05.10
Venus probe fail-
ure.
Approx. 14,000
Unknown
Unknown
Unknown
12 Feb. 1001
89.42
125.2
198.6
05.01
VifillIA probe suceesi
10,380
Unknown
Unknown
Unknown
0 Mitt. 1001
88.20 (Rev.)
114
154 .-
64.87
Successfully recovered
10,1352
Unknown
Unknown '
Unknown
25 Mar. 1001
88.42 (Rev.)
111
154
64.54
.
Successfulfy recovered
10,428.
Unknown.
Unknown.
Unknown.
12 Apr. 11161.
811.00 (Rev.).
110.
188.
65.00.
Successfully recovered
(manned),
• Most of these data are based on Soviet announcements or displays. In a few cases telemetry or other inforinntion ccnfirms experiments or clittn.
•• Not Including the last stage which did not separate In the caso of Sputnik II.
• The meaning of the word "instrumentation" is not known. A weight of 3,257 lbs. seems high for Instrumentation only.
d At 2352Z, 18 May, deorbiting was Initiated, but due to malfunction in the orientation system the vehicle entered a new orbit having cm period of 04.25 min-
utes, a perigee of 190 s.m., and an apogee of 428 e.m.
• A transfer to a higher energy orbit is believed to have occurred during the 18th orbit.

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FOIA release, from the cia-readingroom collection. The PDF is mirrored here; the original link is above. 101 pages are in the text index: search them above, or from the library's search.