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R-12U (8K63M)
Engines:
1. 1 × RD-214
Total mass: 41,750 kg
Apogee: 402 km
Maximum range: 2,150
km
Warhead: 1,600 kg |
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| |
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Kosmos (63S1)
Engines:
1. 1 × RD-214
2. 1 × RD-119
Maximum payload:
LEO: 300 kg
Kosmos-2 (11K63)
Engines:
1. 1 × RD-214
2. 1 × RD-119
Total mass: 48,110 kg
Apogee: 270 km
Maximum payload:
LEO: 450 kg
Launches: 165 (Failures: 21)
/1961-1977/
| |
L |
F |
|
(63S1)
(11K63) |
38
127 |
12
9 |
/1961-1967/
/1965-1977/ |
Payload:
Êîñìîñ, (ÄÑ-1, ÄÑ-2, ÄÑ-Ï1, ÄÑ-À1, ÄÑ-ÌÃ, ÄÑ-ÌÒ, ÄÑ-Ó1, ÄÑ-Ó2, ÄÑ-Ó3, 1ÌÑ, 2ÌÑ, Îìåãà, Ñòðåëà), Èíòåðêîñìîñ (ÄÑ-Ó1, ÄÑ-Ó2, ÄÑ-Ó3) |
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R-14 (8K65)
Engines:
1. 1 × RD-216
Total mass: 48,110
kg
Apogee: 500 km
Warhead: 680
kg
Maximum range: 3,700
km |
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|
| Kosmos 3M (65M-R) suborbital |
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|
Kosmos-1 (65S3)
Engines:
1. 1 × RD-216
2. 1 × 11D49
Total mass: 107,500 kg
Apogee: 400
km
Maximum payload:
LEO: 1,400 kg
Kosmos-3 (11K65)
Engines:
1. 1 × RD-216
2. 1 × 11D49
Total mass: 107,500
kg
Apogee: 250 km
Maximum payload:
LEO: 1,400 kg
Kosmos-3M (11K65M)
Engines:
1. 1 × RD-216M
2. 1 × 11D49
Total mass: 109,000
Apogee: 400 km
Maximum payload:
LEO:
SSO: |
1,400 kg
700 kg
775 kg |
(400 km)
(1,500 km)
(800 km) |
Kosmos-3M (11K65M)
Engines:
1. 1 × RD-216M
2. 1 × 11D49
Total mass: 109,000
Apogee: 400 km
Maximum payload:
LEO:
SSO: |
1,400 kg
700 kg
775 kg |
(400 km)
(1,500 km)
(800 km) |
Kosmos-3M (65M - RB5)
Engines:
1. 1 × RD-216M
2. 1 × 11D49
Launches: 469 (Failures: 24)
/1964-2010/
| |
L |
F |
|
| (65S3) |
8 |
1 |
/1964-1965/ |
| (11K65) |
6 |
2 |
/1966-1968/ |
| (11K65M) |
445 |
20 |
/1967-2010/ |
| (65M-RB5) |
10 |
1 |
/1980-1988/ |
Payload:
(65S3) Ñòðåëà-1
(11K65) Ñòðåëà-2
(11K65M) Öåëèíà-Î, Çàëèâ, Ñôåðà, Èîíîñôåðà, ÄÑ-Ï1-Ì, ÄÑ-Ó2-ÈÏ, ÄÑ-Ó2-Ê, ÄÑ-Ó2-ÈÊ, ÄÑ-Ó2-ÃÊÀ, Ñòðåëà-1Ì, Ñòðåëà-2Ì, Ñòðåëà-3, Ñòðåëà-3Ì, Òàéôóí-1, Òàéôóí-1Á, Òàéôóí-2, Âåêòîð, Ïàðóñ, Îâàë, Öèêàäà, Íàäåæäà, Äóãà-Ê, Èíôîðìàòîð (Îñêàð), ABRIXAS, Megsat, CHAMP, MITA, Rubin, QuickBird, AlSat, Mozhayets, 3-DSI, STSAT, Bilsat, NigeriaSat, UK-DMC, Ìîæàåö, Larets, Òàòÿíà), TopSat, China-DMC, SSETI-Express, Sina, UWE, Gonets-M, SAR-Lupe, Orbcomm
(65M-R) Suborbital payload
(65M-RB5) Áîð-4, Áîð-5 |
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