Soyuz 11A510

In-active

Energia (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 T
  • Thrust
    4037 kN
Family
  • Name
    Soyuz 11A510
  • Family
  • Variant
    11A510
  • Alias
  • Full Name
    Soyuz 11A510
Payload Capacity
  • Launch Cost
  • Low Earth Orbit
    4500 kg
  • Geostationary Transfer Orbit
  • Direct Geostationary
  • Sun-Synchronous Capacity

Energia

Government
None
OKB-1 1946

None

Soyuz 11A510 | US-AO 2

Energia | Russia
Baikonur Cosmodrome, Republic of Kazakhstan
July 20, 1966, 8:58 a.m.
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 Orbit
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Soyuz 11A510 | US-AO 1

Energia | Russia
Baikonur Cosmodrome, Republic of Kazakhstan
Dec. 27, 1965, 10:24 p.m.
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 Orbit
Explore Share

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