Engineering:Kosmos 95

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Short description: Soviet satellite launched in 1965.
Kosmos 95
Mission typeTechnology
COSPAR ID1965-088A
SATCAT no.01706
Mission duration75 days
Spacecraft properties
Spacecraft typeDS-U2-V
ManufacturerYuzhnoye
Launch mass325 kg[1]
Start of mission
Launch date4 November 1965
05:31:00 GMT[2]
RocketKosmos-2M 63S1M
Launch siteKapustin Yar, Site 86/1
ContractorYuzhnoye
End of mission
Decay date18 January 1966
Orbital parameters
Reference systemGeocentric[2]
RegimeLow Earth
Perigee altitude211 km
Apogee altitude521 km
Inclination48.4°
Period91.7 minutes
Epoch4 November 1965
 

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]

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