Kosmos 176
| Mission type | ABM radar target |
|---|---|
| COSPAR ID | 1967-086A |
| Spacecraft properties | |
| Spacecraft type | DS-P1-Yu |
| Manufacturer | Yuzhnoye |
| Launch mass | 250 kilograms (550 lb) |
| Start of mission | |
| Launch date | 12 September 1967, 17:00 UTC |
| Rocket | Kosmos-2I 63SM |
| Launch site | Plesetsk 133/1 |
| End of mission | |
| Decay date | 3 March 1968 |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Perigee | 193 kilometres (120 mi) |
| Apogee | 1,395 kilometres (867 mi) |
| Inclination | 81.9 degrees |
| Period | 100.74 minutes |
Kosmos 176 (Russian: Космос 176 meaning Cosmos 176), also known as DS-P1-Yu No.10 was a Soviet satellite which was used as a radar calibration target for tests of anti-ballistic missiles. It was built by the Yuzhnoye Design Bureau, and launched in 1967 as part of the Dnepropetrovsk Sputnik programme.[1]
A Kosmos-2I 63SM carrier rocket was used to launch Kosmos 176 from Site 133/1 at Plesetsk Cosmodrome.[2] The launch occurred at 17:00 UTC on 12 September 1967, and resulted in Kosmos 176's successful deployment into Low earth orbit.[3]
Kosmos 176 was operated in an orbit with a perigee of 193 kilometres (120 mi), an apogee of 1,395 kilometres (867 mi), 81.9 degrees of inclination, and an orbital period of 100.74 minutes.[1][4] It remained in orbit until it decayed and reentered the atmosphere on 3 March 1968.[4] It was the tenth of seventy nine DS-P1-Yu satellites to be launched,[1] and the ninth of seventy two to successfully reach orbit.[5]
See also
References
- ↑ 1.0 1.1 1.2 Wade, Mark. "DS-P1-Yu". Encyclopedia Astronautica. Retrieved 9 August 2009.
- ↑ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 9 August 2009.
- ↑ Wade, Mark. "Kosmos 2". Encyclopedia Astronautica. Retrieved 9 August 2009.
- ↑ 4.0 4.1 McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 9 August 2009.
- ↑ Krebs, Gunter. "DS-P1-Yu (11F618)". Gunter's Space Page. Retrieved 9 August 2009.
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