A Zenit reentry capsule
| |
| Names | Zenit 2-17 |
|---|---|
| Mission type | Optical imaging reconnaissance |
| Operator | OKB-1 |
| COSPAR ID | 1964-021A  |
| SATCAT no. | 791 |
| Mission duration | 8 days |
| Spacecraft properties | |
| Spacecraft type | Zenit-2 |
| Manufacturer | OKB-1 |
| Launch mass | 4780 kg[1] |
| Start of mission | |
| Launch date | 25 April 1964, 10:19:00 GMT |
| Rocket | Vostok-2 |
| Launch site | Baikonur 31/6 |
| Contractor | OKB-1 |
| End of mission | |
| Disposal | Recovered |
| Landing date | 3 May 1964 |
| Orbital parameters | |
| Reference system | Geocentric[2] |
| Regime | Low Earth |
| Perigee altitude | 203 km |
| Apogee altitude | 296 km |
| Inclination | 65.1° |
| Period | 89.5 minutes |
| Epoch | 25 April 1964 |
Zenit programme
Zenit-2 | |
Kosmos 29 (Russian: Космос 29 meaning Cosmos 29) or Zenit-2 No.17 was a Soviet, a first generation, low resolution, optical film-return reconnaissance satellite which was launched in 1964. A Zenit-2 spacecraft, Kosmos 29 was the seventeenth of eighty-one such satellites to be launched[3] and had a mass of 4,780 kilograms (10,540 lb).
AVostok-2 rocket, serial number R15001-01,[4] was used to launch Kosmos 29. The launch took place at 10:19 GMT on 25 April 1964, using Site 31/6 at the Baikonur Cosmodrome.[5] Following its successful arrival in orbit the spacecraft received its Kosmos designation, along with the International Designator 1964-021A and the Satellite Catalog Number 00791.[6]
Kosmos 29 was operated in a low Earth orbit. On 25 April 1964, it had a perigee of 203 kilometres (126 mi), an apogee of 296 kilometres (184 mi), with inclination of 65.1° and an orbital period of 89.5 minutes. After eight days in orbit, the satellite was deorbited on 3 May 1964 with its return capsule descending by parachute for recovery by Soviet forces.[7][8]
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