|
|
Engines:
1. 8 × H-1 | S-I
2. 1 × J-2 | S-IVB
3. 2 × RL-10A-3-1 | D
Total mass: 605,980
kg
Payload mass:
| |
|
Engines:
1. 8 × H-1 | S-I
2. 1 × HG-3 | MS-IVB-2 (+)
Total mass: 652,440
kg
Payload mass:
|
|
Engines:
0. 4 × M-55 | Minuteman-1
1. 8 × H-1 | S-I
2. 1 × J-2 | S-IVB
Total mass: 689,930
kg
Payload mass:
Status: Study /1965/ |
|
Engines:
0. 4 × UA1205
1. 8 × H-1 | S-I
2. 1 × J-2 | S-IVB
Total mass: 1,511,980
kg
Payload mass:
Status: Study /1965/ |
|
Saturn MLV-1 1.5 (INT-11) |
Engines:
0. 4 × UA1205
1. 8 × H-1 | S-I
2. 1 × J-2 | MS-IVB-1
Total mass: 1,511,980
kg
Payload mass:
Status: Study /1966/ |
|
Saturn MLV-1 1.7 (INT-12) |
Engines:
0. 4 × UA1207
1. 8 × H-1 | S-IB (+)
2. 1 × J-2 | MS-IVB-1
Total mass: 1,959,670
kg
Payload mass:
Status: Study /1966/
|
|
Never flown |
|
|
|
|
|
Engines:
1. 5 × F-1A | MS-IC-1 (+)
2. 5 × J-2 | MS-II-1 (++)
3. 1 × J-2 | MS-IVB-1
Total mass: 3,501,350
kg
Payload mass:
(LEO)
(TLT) |
137,250 kg
49,600 kg |
(185 km) |
Status: Study /1965/ |
|
Engines:
1. 6 × F-1 | MS-IC-1A (+)
2. 7 × J-2 | MS-II-1A (++)
3. 1 × J-2 | MS-IVB-1A
Total mass: 3,648,700 kg
Payload mass:
(LEO)
(TLT) |
145,000 kg
54,400 kg |
(185 km) |
Status: Study /1965/ |
|
Engines:
1. 5 × F-1A | MS- IC-1 (+)
2. 5 × J-2 | MS-II-1 (++)
3. 1 × HG-3 | MS-IVB-2 (+)
Total mass: 3,557,450
kg
Payload mass:
(LEO)
(TLT) |
137,250 kg
53,550 kg |
(185 km) |
Status: Study /1965/ |
|
Engines:
1. 5 × F-1A | MS-IC-1 (+)
2. 5 × HG-3 | MS-II-2 (+++)
3. 1 × HG-3 | MS-IVB-2 (+)
Total mass: 3,664,570
kg
Payload mass:
(LEO)
(TLT) |
160,400 kg
65,800 kg |
(185 km) |
Status: Study /1965/ |
|
Engines:
0. 4 × UA1205
1. 5 × F-1A | S-IC
2. 5 × J-2 | MS-II-4 (+)
3. 1 × J-2 | MS-IVB-1
Total mass: 3,947,350
kg
Payload mass:
(LEO)
(TLT) |
118,000 kg
52,900 kg |
(185 km) |
Status: Study /1965/ |
|
Engines:
0. 4 × UA1205
1. 5 × F-1 | MS-IC-4 (++)
2. 5 × J-2 | MS-II-1 (++)
3. 1 × J-2 | MS-IVB-1
Total mass: 4,615,440
kg
Payload mass:
(LEO)
(TLT) |
160,880 kg
57,500 kg |
(185 km) |
Status: Study /1965/ |
|
Engines:
0. 4 × UA1207
1. 5 × F-1A | MS-IC-1 (+)
2. 5 × J-2 | S-II-1 (++)
3. 1 × J-2 | MS-IVB-1
Total mass: 4,699,860
kg
Payload mass:
(LEO)
(TLT) |
171,990 kg
63,160 kg |
(185 km) |
Status: Study /1967/
|
|
Never flown |
|
|
|
Engines:
0. 4 × UA1207
1. 5 × F-1 | MS-IC-4 (++)
2. 7 × J-2 | MS-II-1A (+++)
3. 1 × J-2 | MS-IVB-1A (+)
Total mass: 5,172,820
kg
Payload mass:
(LEO)
(TLT) |
200,000 kg
67,000 kg |
(185 km) |
Status: Study /1966/ |
|
Never flown |
|
|
|
|
|
Engines:
0. 4 × UA 156
1. 5 × F-1А | MS-IC-25 (+++)
2. 5 × J-2 | MS-II-4 (+)
3. 1 × J-2 | MS-IVB-1A (+)
Total mass: 6,342,540
kg
Payload mass:
(LEO) 223,500 kg (185 km)
Status: Study /1967/ |
|
Engines:
0. 4 × UA 156
1. 5 × F-1 | MS-IC-25 (+++)
2. 5 × J-2 | MS-II-4 (+)
3. 1 × NERVA
Total mass:
Payload mass:
(LEO) 248,663 kg (185 km)
Status: Study /1968/
|
|
Never flown |
|
|
|
|
|
Engines:
0. 4 × FL
1. 5 × F-1 / MS-IC-260 / (+)
2. 5 × HG-3 | MS-II-2 (+++)
Total mass: 10,351,050 kg
Payload mass:
(LEO) 362,700 kg (185 km)
Status: Study /1967/ |
|
Engines:
1. 8 × F-1 | 2 x LRB-23
1. 5 × F-1 | MS-IC-1 (+)
2. 5 × J-2 | MS-II-4 (+)
3. 1 × J-2 | MS-IVB-1A (+)
Total mass: 7,178,900 kg
Payload mass:
(LEO)
(TLT) |
262,670 kg
99,850 kg |
(185 km) |
Status: Study /1967/ |
|
Engines:
1. 8 × F-1 | 2 x LRB-23
1. 5 × F-1A | MS-IC-1 (+)
2. 5 × HG-3 | MS-II-2 (+++)
3. 1 × HG-3 | MS-IVB-2 (+)
Total mass: 7,386,760 kg
Payload mass:
(LEO)
(TLT) |
435,300 kg
185,900 kg |
(185 km) |
Status: Study /1967/ |
|
Never flown |
|
|
|
|
Engines:
1. 2 × SRM (SRB)
2. 3 × RS-25 (SSME)
2. 2 × AJ10-190 (OME)
3. 2 × RL-10A-3A | Centaur-T
Payload mass: |
(LEO) |
24,000
kg (204 km, 28.5) |
|
(GSO) |
4,500
kg (G)
6,300 kg (G Prime) |
|
|
Payload: Deep space probes |
|
|
Never flown |
|
|
Space Shuttle-Centaur |
|
|
|
|
|
|
Engines:
1. 2 × SRB
2. 3 × RS-25 (SSME)
3. 2 × AJ10-190 (OME)
Total mass: 1,966,675 kg
Payload mass:
(LEO) 77,000 kg
(400 km, 28,5) |
|
Engines:
1. 2 × SRB
2. 2 × RS-25 (SSME)
3. 2 × AJ10-190 (OME)
Total mass: 1,966,675 kg
Payload mass:
(LEO) 47,000 kg (400 km)
(LEO) 52,000 kg (300 km) |
|
Never flown |
|
|
Ares 1-X
Engines:
1. 1 × RSRB-4 + segment
2. dummy
3. dummy |
|
Launches: 1 (Failures: 0)
/2009/ |
|
Retired |
|
|
Engines:
1. 1 × RSRB-5 (SRB)
2. dummy
3. dummy |
|
Engines:
1. 1 × RSRB-5 (SRB)
2. 1 × J-2X
3. 1 × AJ10-190 (OME) / CEV
Total mass: 907,000 kg
Payload mass:
ISS: |
25,000 kg |
(400 km, 51,6) |
|
|
Payload: Orion Multi-Purpose Crew Vehicle (Constellation program) |
|
|
Never flown |
|
|
|
|
Ares 1 |
|
|
|
|
|
|
|
Engines:
1. 2 × RSRB-5 (SRB)
2. 5 × RS-68
3. 1 × J-2X
Total mass: 3,360,000 kg
Payload mass:
(LEO)
(TLT) |
124,600 kg (160 km, 28.5)
54,600 kg |
|
|
Payload: Altair lunar lander (Constellation program) |
|
|
Never flown |
|
|
|
Ares 5 |
|
|
|
|
|
Neutron |
|
|
|
|
Engines:
1. 9 × Archimedes
2. 1 × Archimedes vac
Total mass: 480,000 kg
Payload mass:
(LEO) |
|
|
15,000 kg
13,000 kg
8,000 kg
|
(reusable )
(reusable to pad)
|
|
|
|
Never flown |
|
|
|
|