Engineering:Kosmos 51

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Kosmos 51
Mission typeTechnology
Cosmic ray
OperatorVNIIEM
COSPAR ID1964-080A
SATCAT no.00947
Mission duration340 days
Spacecraft properties
Spacecraft typeDS-MT
ManufacturerYuzhnoye
Launch mass350 kg[1]
Start of mission
Launch date9 December 1964
23:02:00 GMT
RocketKosmos-2I 63S1
Launch siteKapustin Yar, Site 86/1
ContractorYuzhnoye
End of mission
Decay date14 November 1965
Orbital parameters
Reference systemGeocentric[2]
RegimeLow Earth
Perigee altitude262 km
Apogee altitude533 km
Inclination48.8°
Period92.5 minutes
Epoch9 December 1964
 

Kosmos 51 (Russian: Космос 51 meaning Cosmos 51), also known as DS-MT No.3 was a technology demonstration satellite which was launched by the Soviet Union in 1964 as part of the Dnepropetrovsk Sputnik programme. Its primary mission was to demonstrate an electric gyrodyne orientation system.[3] It also carried a scientific research package as a secondary payload, which was used to study cosmic rays and the luminosity of the stellar background.

It was launched aboard a Kosmos-2I 63S1 rocket[4] from Site 86/1 at Kapustin Yar. The launch occurred at 23:02 GMT on 9 December 1964.[5]

Kosmos 51 was placed into a low Earth orbit with a perigee of 262 kilometres (163 mi), an apogee of 533 kilometres (331 mi), 48.8° of inclination, and an orbital period of 92.5 minutes. It decayed from orbit on 14 November 1965.[6] Kosmos 51 was the last of three DS-MT satellites to be launched. The first was lost in a launch failure on 1 June 1963, and the second was launched as Kosmos 31 on 6 June 1964.[7]

See also

  • 1964 in spaceflight

References