cosmos.wikisort.org - Spacecraft
Kosmos 95 (Russian: Космос 95 meaning Cosmos 95), also known as DS-U2-V No.2, was a Soviet satellite which was launched in 1965 as part of the Dnepropetrovsk Sputnik programme. The spacecraft weighed 325 kilograms (717 lb),[3] and was built by the Yuzhnoye Design Office, and was used to conduct classified technology development experiments for the Soviet armed forces.[3]
| Mission type | Technology |
|---|---|
| COSPAR ID | 1965-088A |
| SATCAT no. | 01706 |
| Mission duration | 75 days |
| Spacecraft properties | |
| Spacecraft type | DS-U2-V |
| Manufacturer | Yuzhnoye |
| Launch mass | 325 kg[1] |
| Start of mission | |
| Launch date | 4 November 1965 05:31:00 GMT[2] |
| Rocket | Kosmos-2M 63S1M |
| Launch site | Kapustin Yar, Site 86/1 |
| Contractor | Yuzhnoye |
| End of mission | |
| Decay date | 18 January 1966 |
| Orbital parameters | |
| Reference system | Geocentric[2] |
| Regime | Low Earth |
| Perigee altitude | 211 km |
| Apogee altitude | 521 km |
| Inclination | 48.4° |
| Period | 91.7 minutes |
| Epoch | 4 November 1965 |
A Kosmos-2M 63S1M[4] carrier rocket was used to launch Kosmos 95 into low Earth orbit. The launch took place from Site 86/1 at Kapustin Yar.[5] The launch occurred at 05:31 GMT on 4 November 1965, and resulted in the successful insertion of the satellite into orbit.[6] Upon reaching orbit, the satellite was assigned its Kosmos designation, and received the International Designator 1965-088A. The North American Air Defense Command assigned it the catalogue number 01706.[7]
Kosmos 95 was the second of four DS-U2-V satellites to be launched.[3][8] It was operated in an orbit with a perigee of 211 kilometres (131 mi), an apogee of 521 kilometres (324 mi), an inclination of 48.4°, and an orbital period of 91.7 minutes.[9] On 18 January 1966, it decayed from orbit and reentered the atmosphere.[9][10]
See also
- 1965 in spaceflight
References
- https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=1965-088A - 27 February 2020
- https://nssdc.gsfc.nasa.gov/nmc/spacecraft/displayTrajectory.action?id=1965-088A - 27 February 2020
- Wade, Mark. "DS-U2-V". Encyclopedia Astronautica. Archived from the original on 5 January 2009. Retrieved 6 December 2009.
- Wade, Mark (31 October 2001). "Kosmos 63S1M". Encyclopedia Astronautica. Retrieved 14 January 2010.
- McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 6 December 2009.
- Wade, Mark. "Kosmos 2". Encyclopedia Astronautica. Archived from the original on 18 June 2012. Retrieved 6 December 2009.
- "Cosmos 95". NSSDC Master Catalog. US National Space Science Data Center. Retrieved 6 December 2009.
- Krebs, Gunter. "DS-U2-V". Gunter's Space Page. Retrieved 6 December 2009.
- McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 6 December 2009.
- "World Civil Satellites 1957-2006". Space Security Index. Archived from the original on 18 July 2011. Retrieved 6 December 2009.
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На других языках
- [en] Kosmos 95
[ru] Космос-95
Ко́смос-95 («ДС-У2-В» № 2) — второй советский научно-исследовательский спутник серии космических аппаратов «Космос» типа «ДС-У2-В», запущенный для комплексного исследования ионосферы Земли и вибрационных нагрузок на КА при шахтном пуске ракеты-носителя.[2]Другой контент может иметь иную лицензию. Перед использованием материалов сайта WikiSort.org внимательно изучите правила лицензирования конкретных элементов наполнения сайта.
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