|
|
 |
Engines:
0. 6 × RD-270
1. 3 × RD-270
2. 3 × RD-254
3. 3 × 11D423
Total mass:
4,823,000 kg
Payload mass:
(LEO) 151,000 kg
(200 km, 51 )
(TLT) 50,000 kg
|
|
Engines:
0. 6 × RD-270
1. 3 × RD-270
3. 9 × RD-54
Total mass:
4,790,000 kg
Payload mass:
(LEO) 185,000 kg
|
|
Engines:
0. 6 × RD-270
1. 3 × RD-270
2. 3 × RD-350
Total mass:
4,800,000 kg
Payload mass:
(LEO) 215,000 kg
|
 |
Never flown |
|
| |
|
| Ur-700 |
 |
|
 |
|
| |
|
Engines:
0. 6 × RD-270
1. 3 × RD-270
2. 7 × RD-04111 (RO-3)
3. 3 × RD-04111 (RO-3)
Total mass:
4,823,000 kg
Payload mass:
(LEO) 230,000-270,000 kg
(200 km, 51)
(IPT) 105,000-115,000 kg
|
|
Never flown |
|
| |
|
| |
 |
N1 (11A52) - L3
Engines:
1. 30 × NK-15
2. 8 × NK-15v
3. 4 × NK-21
4. 1 × NK-19
5. 1 × RD-58 | Bl. D
Total mass: 2,735,000 kg
Payload mass:
(LEO)
(TLT) |
95,000 kg
23,500 kg |
|
 |
Launches >>
|
 |
Retired |
|
|
|
|
| N1 |
 |
|
|
|
|
Engines:
1. 24 × NK-15
2. 8 × NK-15v
3. 4 × NK-21
4. 1 × NK-19
Total mass: 2,110,000 kg
Payload mass:
(LEO) 75,000 kg
Status: Study /1962/
|
|
Engines:
1. 30 × NK-15
2. 8 × NK-15v
3. 4 × NK-21
4. 1 × NK-19
5. 1 × RD-58 | Bl. D
Total mass: 2,735,000 kg
Payload mass:
(LEO)
(TLT) |
95,000 kg
23,500
kg |
|
 |
Payload:
(LEO)
ÒÊÑ-1961
OÏ-1962
ÎÑ-1-1965
ÎÑ-1-1969
ÌÊÁÑ-1971
(Moon)
7Ê-ËÎÊ + Ë3
19K / êîìïëåêñ
21K / òàíêåð
Ë3Ì-1970
(Intrplanetary)
4ÍÌ / ìàðñîõîä
5ÍÌ / Ìàðñ ãðóíò |
|
|
Never flown |
|
|
|
Engines:
1. 30 × NK-33
2. 8 × NK-43
3. 4 × NK-39
4. 1 × NK-39 | Bl. V
5. 1 × RD-58 | Bl. D
Total mass: 3,025,000 kg
Payload mass:
(LEO) 105,000 kg
Status: Development
/cancelled 1974/ |
|
Engines:
1. 30 × NK-33
2. 8 × NK-43
3. 4 × NK-39
4. 2 × RD-56M | Bl. SR
Total mass: 2,677,900 kg
Status: Development
/cancelled 1974/ |
|
Engines:
1. 30 × NK-33
2. 8 × NK-43
3. 2 × RD-57 | Bl. S
4. 1 × RD-56M | Bl. R
Total mass: 2,773,000 kg
Status: Development
/cancelled 1971/ |
|
Engines:
1. 30 × NK-15
2. 6 × RD-57
3. 2 × RD-57 | Bl. S
4. 1 × RD-56M | Bl. R
Total mass: 2,348,000 kg
Status: Development
/cancelled 1974/ |
|
Engines:
1. 24 × NK-15
2. 20 × YaRD Type V
Total mass: 2,600,000 kg
Payload mass:
(LEO) 420,000 kg
(lunar surface) 38,500
kg
Status: Study /1963/ |
|
Launches: 0
Payload:
(LEO)
ÌÊÁÑ-1971
(Moon)
Ë3Ì-1970
Ë3Ì-1972
Ë5 / ëóíîõîä |
|
|
Never flown |
|
|
|
Engines:
1. 6 × RD-170
8 × RD-170
2. 4 × RD-0120
2. 1 × RD-57M
Payload mass:
(LEO)
200,000 kg (200
km, 50,7)
172,000 kg (200
km, 97)
(GSO)
(TLT)
(TMT) |
36,000 kg
43,000 kg
52,000 kg |
|
|
Payload:
LEK (Lunar Expeditionary Complex), Lunokhod LEK, LZhM, LZM |
|
|
Never flown |
|
| |
|
| Vulkan |
|
|
|
| |
|
Engines:
|
|
Payload:
LK Energia, LOK Energia, Mars 1989, Mars 1994, Mir-2, EA, USB, 37KS, LO, NPG, OK-M2, Ozone Replenishment Satellite, Nuclear Waste Disposal, Geostationary Platform, Orbital Debris Remover, Polar City Illuminator, 37KB, KRT-25 Radio Telescope, ERTA, Ecosat
|
|
|
|
Never flown |
|
| |
|
|
|
|
Energia
Engines:
Total mass: 2,524,600 kg
Payload mass:
| (LEO) |
| 88,000 kg |
(TKS) |
|
| 105,000 kg |
(Buran) |
|
|
|
Launches >>
|
Payload: Ïîëþñ (Ñêèô-ÄÌ), Áóðàí ÎÊ |
|
|
Retired |
|
|
|
| Energia |
|
|
|
|
|
|
|
|
Engines:
1. 2 × RD-180
2. 1 × RD-0120M
Total mass:
1,022,800 kg
Payload mass:
(LEO) 34,000 kg |
|
Never flown |
|
| |
| Energia M |
|
|
|
|
| |
|
Engines:
0. An 225 (aircraft)
0. 1 × An-225
2. 1 × RD-701
Total mass: 265,000 kg
Payload mass:
(LEO)
6,600 kg
9,500 kg |
(400 km,90)
(200 km, 51) |
Status: Study /1988/ |
|
Never flown |
|
|
| MAKS |
|
|
|
|
|
Never flown |
|
|
|
|
|
