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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 3
SOVIET SPACE PROBES
LUNIIC I b VENUS PROBE dLUNIIC II b. LUNII: Ill I.
(1959 THETA)
Weight (lbs.) 1418.
Configuration Diameter (ft.)
and Length (ft.) of Satel-
lite.
Cylinder with hemispherical
end. length 6.67 feet, diem.
eter 3.4 . 1 feet,
Date ',switched
Orbit Period
12 February 1901.
Not yet determinable.
797 858 959
A portion of the experitnentation weight was affixed to the last stage rocket bodies, and it por-
tion In special containers— a 2.7 foot diameter ejectable sphere in tjte case of Luniks I and II
and a cylinder— truncated cone in the case of Lttnik III, which was probably also separated.
The last stago of all three Luniks was probably essentially the same as that displayed at
New York and other expositions.
Shape: A cone and cylinder, 17•6 feet long, 8•6 feet In diameter. Weight of empty last
stage including instrumentation: varying slightly, about 3,250-3,400 pounds.
2 January 1950 12 September 1050 4 October 1959
450 Days (around the sitn).. Impacted on moon Approx. 19 days (around the
earth).
Approx. :30,000
Approx. 200,000
Approx. 75
Perigee (et. mi.)
Apogee (st. mi.)
Inclination to Equator
(degrees).
Contents
Not yet detertninablv.
Not yet (Interminable.
0.55 to the ecliptic.
Large variety of research in-
struments, chemica l bat-
teries, transmitters.
Equipment for measuring mi.
erometeerold impacts, nature
or !Tact: matter. co .iitole nu.
rIlation. magnetic fields. •
Equipment for temperature,
gravitation. radiation, and
photography eiNperitnent.,
Instruments for measuring
magnetic field of earth and
:noon, cosmic rays, meteor-
ites, density of matter In
space, radiation around
earth and moon.
Radio Frequencies Used,
MCS.
183.0
10.001
183 0
10.093
183.0
10 080
922.9.
10.005 19.997 71
10 . 007 20.003 70
39.086
71
70
Putt of Last Signal Inter. Soviet:, reported 02 hour. 38.4 hours of reception 'twirl.: Unknown. US• 22 February 1961.
cept.
Date of Satellite 1)emire. •
ceptIon.
Indefinite around Slta 2192:24Z-13 September 1959.
Sibly 18 October 1959,
UnIsnown (nth:finite around the stun.
• Most of these data sire hi sed on Soviet Announcements o displays. In it few eases telemetry or other informatio u confirms experiments or dent.
The \Vest's capability to Intercept transmissions from a Soviet lunar probe, especially in the lower freitnencies, is very limited. Additionally, the Soviet.
probably trigger the transmitters while over Soviet territory, and pass only limited position data to the West.
• The earth satellite designation assigned Ltmlk III.
d Launched from a 14,300 lb. earth satellite vehicle.
• A primary purpose of this event Ti t( i.e., to check Injection systeins, propulsion and gnid3nee, and racli communications Over lonw

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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.