| Mission type | ABM radar target |
|---|---|
| COSPAR ID | 1967-086A |
| SATCAT no. | 02942 |
| Mission duration | 173 days |
| Spacecraft properties | |
| Spacecraft type | DS-P1-Yu |
| Manufacturer | Yuzhnoye |
| Launch mass | 400 kg [1] |
| Start of mission | |
| Launch date | 12 September 1967 17:00:00 GMT |
| Rocket | Kosmos-2I 63SM |
| Launch site | Plesetsk, Site 133/3 |
| Contractor | Yuzhnoye |
| End of mission | |
| Decay date | 3 March 1968 |
| Orbital parameters | |
| Reference system | Geocentric [2] |
| Regime | Low Earth |
| Perigee altitude | 196 km |
| Apogee altitude | 1525 km |
| Inclination | 81.9° |
| Period | 102.5 minutes |
| Epoch | 12 September 1967 |
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 a 400 kilograms (880 lb) spacecraft, [1] was built by the Yuzhnoye Design Office, and launched in 1967 as part of the Dnepropetrovsk Sputnik programme. [3]
A Kosmos-2I 63SM carrier rocket was used to launch Kosmos 176 from Site 133/3 at Plesetsk Cosmodrome. [4] The launch occurred at 17:00:00 GMT on 12 September 1967, and resulted in Kosmos 176's successful deployment into low Earth orbit. [5] Upon reaching orbit, it was assigned its Kosmos designation, and received the International Designator 1967-086A. [1]
Kosmos 176 was operated in an orbit with a perigee of 196 kilometres (122 mi), an apogee of 1,525 kilometres (948 mi), an inclination of 81.9°, and an orbital period of 102.5 minutes. [2] It remained in orbit until it decayed and reentered the atmosphere on 3 March 1968. [6] It was the tenth of seventy nine DS-P1-Yu satellites to be launched, [3] and the ninth of seventy two to successfully reach orbit. [7]
See also
References
- ^
a
b
c
"Cosmos 176: Display 1967-086A". nssdc.gsfc.nasa.gov. NASA. 27 February 2020. Retrieved 18 April 2020.
This article incorporates text from this source, which is in the
public domain.
- ^
a
b
"Cosmos 176:Trajectory 1967-086A". nssdc.gsfc.nasa.gov. NASA. 27 February 2020. Retrieved 18 April 2020. This article incorporates text from this source, which is in the
public domain.
- ^ a b Wade, Mark. "DS-P1-Yu". Encyclopedia Astronautica. Archived from the original on 2 June 2012. Retrieved 9 August 2009.
- ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 9 August 2009.
- ^ Wade, Mark. "Kosmos 2". Encyclopedia Astronautica. Archived from the original on 18 June 2012. Retrieved 9 August 2009.
- ^ 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.
 | This article about one or more spacecraft of the Soviet Union is a stub. You can help Wikipedia by expanding it. |
| Mission type | ABM radar target |
|---|---|
| COSPAR ID | 1967-086A |
| SATCAT no. | 02942 |
| Mission duration | 173 days |
| Spacecraft properties | |
| Spacecraft type | DS-P1-Yu |
| Manufacturer | Yuzhnoye |
| Launch mass | 400 kg [1] |
| Start of mission | |
| Launch date | 12 September 1967 17:00:00 GMT |
| Rocket | Kosmos-2I 63SM |
| Launch site | Plesetsk, Site 133/3 |
| Contractor | Yuzhnoye |
| End of mission | |
| Decay date | 3 March 1968 |
| Orbital parameters | |
| Reference system | Geocentric [2] |
| Regime | Low Earth |
| Perigee altitude | 196 km |
| Apogee altitude | 1525 km |
| Inclination | 81.9° |
| Period | 102.5 minutes |
| Epoch | 12 September 1967 |
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 a 400 kilograms (880 lb) spacecraft, [1] was built by the Yuzhnoye Design Office, and launched in 1967 as part of the Dnepropetrovsk Sputnik programme. [3]
A Kosmos-2I 63SM carrier rocket was used to launch Kosmos 176 from Site 133/3 at Plesetsk Cosmodrome. [4] The launch occurred at 17:00:00 GMT on 12 September 1967, and resulted in Kosmos 176's successful deployment into low Earth orbit. [5] Upon reaching orbit, it was assigned its Kosmos designation, and received the International Designator 1967-086A. [1]
Kosmos 176 was operated in an orbit with a perigee of 196 kilometres (122 mi), an apogee of 1,525 kilometres (948 mi), an inclination of 81.9°, and an orbital period of 102.5 minutes. [2] It remained in orbit until it decayed and reentered the atmosphere on 3 March 1968. [6] It was the tenth of seventy nine DS-P1-Yu satellites to be launched, [3] and the ninth of seventy two to successfully reach orbit. [7]
See also
References
- ^
a
b
c
"Cosmos 176: Display 1967-086A". nssdc.gsfc.nasa.gov. NASA. 27 February 2020. Retrieved 18 April 2020. This article incorporates text from this source, which is in the
public domain.
- ^
a
b
"Cosmos 176:Trajectory 1967-086A". nssdc.gsfc.nasa.gov. NASA. 27 February 2020. Retrieved 18 April 2020. This article incorporates text from this source, which is in the
public domain.
- ^ a b Wade, Mark. "DS-P1-Yu". Encyclopedia Astronautica. Archived from the original on 2 June 2012. Retrieved 9 August 2009.
- ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 9 August 2009.
- ^ Wade, Mark. "Kosmos 2". Encyclopedia Astronautica. Archived from the original on 18 June 2012. Retrieved 9 August 2009.
- ^ 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.
| This article about one or more spacecraft of the Soviet Union is a stub. You can help Wikipedia by expanding it. |