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Omega
Part of DS
Cosmos 14 Credit: Manufacturer Image |
Russian technology satellite. Early Cosmos satellite, evidently using the Yuzhnoye DS satellite bus. Payload developed by the VNIIEM to test electric gyrodyne orientation systems. Technology satellite, Russia. Launched 1963.
Status: Operational 1963. First Launch: 1963-04-13. Last Launch: 1963-12-13. Number: 2 . Gross mass: 347 kg (765 lb).
More at: Omega.
Family:
Technology,
Technology satellite.
Country:
Russia.
Launch Vehicles:
Kosmos 2,
R-12,
Kosmos 63S1.
Launch Sites:
Kapustin Yar,
Kapustin Yar Mayak-2.
Agency:
MO,
VNIIEM.
Bibliography:
2,
6,
12915.
1963 April 13 - .
11:00 GMT - .
Launch Site:
Kapustin Yar.
Launch Complex:
Kapustin Yar Mayak-2.
LV Family:
R-12.
Launch Vehicle:
Kosmos 63S1.
- Cosmos 14 - .
Payload: DS-U / Omega-1. Mass: 347 kg (765 lb). Nation: Russia.
Agency: MO.
Class: Technology.
Type: Navigation technology satellite. Spacecraft Bus: DS.
Spacecraft: Omega.
Decay Date: 1963-08-29 . USAF Sat Cat: 567 . COSPAR: 1963-010A. Apogee: 410 km (250 mi). Perigee: 250 km (150 mi). Inclination: 48.90 deg. Period: 91.10 min. Tested VNIIEM electric gyrodyne satellite orientation technology..
1963 December 13 - .
14:15 GMT - .
Launch Site:
Kapustin Yar.
Launch Complex:
Kapustin Yar Mayak-2.
LV Family:
R-12.
Launch Vehicle:
Kosmos 63S1.
- Cosmos 23 - .
Payload: DS-U / Omega-1. Mass: 347 kg (765 lb). Nation: Russia.
Agency: MO.
Class: Technology.
Type: Navigation technology satellite. Spacecraft Bus: DS.
Spacecraft: Omega.
Decay Date: 1964-03-27 . USAF Sat Cat: 707 . COSPAR: 1963-050A. Apogee: 560 km (340 mi). Perigee: 232 km (144 mi). Inclination: 48.90 deg. Period: 92.40 min. Tested VNIIEM electric gyrodyne satellite orientation technology..
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