Kosmos 13 (Russian: Космос 13 meaning Cosmos 13) or Zenit-2 No.9 was a Soviet optical film-return reconnaissance satellite launched in 1963. A Zenit-2 spacecraft, Kosmos 13 was the eighth of eighty-one such satellites to be launched.[3][4]
Mission type | Optical imaging reconnaissance Radiation |
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COSPAR ID | 1963-006A ![]() |
SATCAT no. | 00554 |
Mission duration | 8 days |
Spacecraft properties | |
Spacecraft type | Zenit-2 |
Manufacturer | OKB-1 |
Launch mass | 4730 kg[1] |
Start of mission | |
Launch date | 21 March 1963, 08:24:00 GMT |
Rocket | Vostok-2 s/n T15000-01 |
Launch site | Baikonur, Site 1/5 |
Contractor | OKB-1 |
End of mission | |
Disposal | Recovered |
Landing date | 29 March 1963 |
Landing site | Steppe in Kazakhstan |
Orbital parameters | |
Reference system | Geocentric[2] |
Regime | Low Earth |
Perigee altitude | 192 km |
Apogee altitude | 324km |
Inclination | 65.0° |
Period | 89.8 minutes |
Epoch | 21 March 1963 |
Kosmos 13 was a Zenit-2 satellite, a first generation, low resolution, reconnaissance satellite derived from the Vostok spacecraft used for crewed flights, the satellites were developed by OKB-1. In addition to reconnaissance, it was also used for research into radiation in support of the Vostok programme. It had a mass of 4,730 kilograms (10,430 lb).[1]
The Vostok-2 rocket, serial number T15000-01,[5] was used to launch Kosmos 13. The launch took place from Site 1/5 at the Baikonur Cosmodrome at 08:24:00 GMT on 21 March 1963.[2] Following its successful arrival in orbit the spacecraft received its Kosmos designation, along with the International Designator 1963-006A and the Satellite Catalog Number 00554.[1]
Kosmos 13 was operated in a low Earth orbit. On 23 March 1963 it had a perigee of 192 kilometres (119 mi), an apogee of 324 kilometres (201 mi), with an inclination of 65.0°, and an orbital period of 89.8 minutes.[2] After eight days in orbit, the spacecraft was deorbited on 29 March 1963, with its return capsule descending by parachute for recovery by the Soviet forces in the steppe in Kazakhstan.[2] In addition to its reconnaissance payload, Kosmos 13 also carried an experiment to measure radiation levels in its environment.[4]
← 1962 · Orbital launches in 1963 · 1964 → | |
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Luna E-6 No.2 | OPS 0048 | OPS 0180 | Luna E-6 No.3 | Syncom 1 | OPS 0240 | OPS 0583 | OPS 0627 · P-11 No.1 | Kosmos 13 | OPS 0720 | Luna 4 | Explorer 17 | Transit 5A-2 | DS-P1 No.2 | Kosmos 14 | Kosmos 15 | OPS 1008 | OPS 1298 | Kosmos 16 | Telstar 2 | Midas 7 · DASH 1 · ERS-5 · ERS-6 · Westford 2 | Mercury-Atlas 9 (Balloon Subsatellite 2 · Flashing Light Unit) | OPS 0924 | Kosmos 17 | Kosmos 18 | DS-MT No.1 | OPS 0954 | Midas 8 · ERS-7 · ERS-8 | Vostok 5 | FTV-1292 · Solrad 6 · LOFTI 2A · Surcal 3 · Radose 112 | Transit 5A-3 | Vostok 6 | TIROS-7 | OPS 0999 · Hitchhiker 1 | GRS | OPS 1440 | Zenit-2 No.12 | OPS 1467 | OPS 1266 | Midas 9 · DASH 2 · ERS-9 · ERS-10 | Syncom 2 | OPS 1370 | Kosmos 19 | DS-A1 No.3 | OPS 1419 | OPS 1561 · LAMPO | OPS 1947 | OPS 1353 | OPS 1610 | Transit 5BN-1 · Transit 5E-1 | Vela 1A · Vela 1B · ERS-12 | Kosmos 20 | DS-A1 No.4 | OPS 2196 | OPS 2437 · Hitchhiker 2 | Polyot 1 | OPS 2268 | Kosmos 21 | Kosmos 22 | Explorer 18 | Atlas-Centaur 2 | OPS 2260 | Zenit-2 No.14 | Transit 5BN-2 · Transit 5E-2 | Kosmos 23 | OPS 2372 | Kosmos 24 | Explorer 19 | TIROS-8 | OPS 1388 · Hitchhiker 3 | |
Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated in underline. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in brackets. |
Zenit-2 satellites | |
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Zenit-2 |
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Zenit-2M (Gektor) |
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