|
|
 |
Engines:
0. 6 × RD-270
1. 3 × RD-270
2. 3 × RD-254
3. 3 × 11D423
Total mass: 4,823,000 kg
Payload:
(200 km, 51 ) 151,000 kg (TLT) 50,000 kg
|
|
Engines:
0. 6 × RD-270
1. 3 × RD-270
3. 9 × RD-54
Total mass: 4,790,000 kg
Payload (LEO): 185,000 kg
|
|
Engines:
0. 6 × RD-270
1. 3 × RD-270
2. 3 × RD-350
Total mass: 4,800,000 kg
Payload (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:
(LEO)
(IPT) |
230,000-270,000 kg
105,000-115,000 kg
|
|
|
Never flown |
|
| |
|
| |
 |
Total mass: 2,735,000 kg
Payload:
(LEO)
(TLT) |
95,000 kg
23,500 kg |
|
|
 |
Launches: 4 (Failures: 4)
/1969-1972/
 |
|
S5.92 | KTDU-53 |
|
 |
Retired |
|
|
|
|
|
| N1 |
 |
|
|
|
|
Total mass: 2,110,000 kg
Payload:
(LEO) 75,000 kg
Status: Study /1962/
|
|
Total mass: 2,735,000 kg
Payload:
(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 |
|
|
|
Total mass: 3,025,000 kg
Payload (LEO): 105,000 kg
Status: Development
/cancelled 1974/ |
|
Total mass: 2,677,900 kg
Status: Development
/cancelled 1974/ |
|
Total mass: 2,773,000 kg
Status: Development
/cancelled 1971/ |
|
| Engines: |
1.
2.
3.
4.
|
30 ×
6 ×
2 ×
1 × |
NK-15
RD-57
RD-57 | Bl. S
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:
(LEO) 420,000 kg
(lunar surface) 38,500
kg
Status: Study /1963/ |
|
Payload:
(LEO)
ÌÊÁÑ-1971
(Moon)
Ë3Ì-1970
Ë3Ì-1972
Ë5 / ëóíîõîä |
|
|
Never flown |
|
|
|
Payload (LEO):
200,000 kg (200
km, 50,7)
172,000 kg (200
km, 97)
Payload:
(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 |
|
|
| |
|
|
|
 |
Energia
Engines:
Total mass: 2,524,600
Payload:
| 88,000 kg |
(TKS) |
|
| 105,000 kg |
(Buran) |
|
|
|
Launches: 2 (Failures: 1)
/1987-1988/
 |
2 × RD-58 | Buran
2 × 11D442 | TKS |
|
|
Retired |
|
|
|
| Energia |
|
|
|
|
|
|
|
|
Engines:
1. 2 × RD-180
2. 1 × RD-0120M
Total mass: 1,022,800 kg
Payload (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 (LEO):
6,600 kg
9,500 kg |
(400 km,90)
(200 km, 51) |
Status: Study /1988/ |
|
Never flown |
|
|
| MAKS |
|
|
|
|
|
