Soyuz 11A510
In-activeEnergia (OKB-1)
Dec. 27, 1965
Description
The Soyuz/Vostok, also known as just Soyuz or Vostok, or by its GRAU index, 11A510 was an interim expendable carrier rocket used by the Soviet Union in 1965 and 1966. Two were launched with prototype US-A satellites.
Specifications
-
Stages
3 -
Length
31.0 m -
Diameter
10.3 m -
Fairing Diameter
― -
Launch Mass
275.0 T -
Thrust
4037.0 kN
Family
-
Name
Soyuz 11A510 -
Family
― -
Variant
11A510 -
Alias
― -
Full Name
Soyuz 11A510
Payload Capacity
-
Launch Cost
― -
Low Earth Orbit
4500.0 kg -
Geostationary Transfer
Orbit
― -
Direct Geostationary
― -
Sun-Synchronous Capacity
―
Energia
Government
None
OKB-1 1946None
Soyuz 11A510 | US-AO 2
Energia | RussiaBaikonur Cosmodrome, Republic of Kazakhstan
Status: Launch Successful
Mission:
US-A (Upravlenniye Sputnik Aktivny) were active radar satellites for ocean surveillance. The high power consumtion of the active radar required a nuclear reactor as power source. The satellites were known as RORSAT in the west. The US-AO series consisted of satellites, which tested all the system components but the nuclear reactor. They were battery powered.
Low Earth OrbitSoyuz 11A510 | US-AO 1
Energia | RussiaBaikonur Cosmodrome, Republic of Kazakhstan
Status: Launch Successful
Mission:
US-A (Upravlenniye Sputnik Aktivny) were active radar satellites for ocean surveillance. The high power consumtion of the active radar required a nuclear reactor as power source. The satellites were known as RORSAT in the west. The US-AO series consisted of satellites, which tested all the system components but the nuclear reactor. They were battery powered.
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