USA

Saturn 1 Bl. 2

Bl. 1

Saturn 1 Bl. 1
Engines:
1. 8 ×  H-1 | S-I
2.         dummy  | S-4

Total mass: 420,000 kg
Apogee: 185 km

Fairing:

(1)
(2)

SA 1-3
SA 4

Saturn 1 Bl. 2
Engines:
1. 8 ×  H-1 | S-I
2. 6 × RL-10  | S-4

Total mass: 509,660 kg
Apogee: 510 km
Payload (LEO): 9,000 kg

Fairing:

(3)
(4)

SA 5
SA 6-10

Launches: 10 (Failures: 0)
/1961-1965/

	L	F
(Bl.1) (Bl.2)	4 6		/1961-1963/ /1964-1965/

Payload:
(Block 1) Highwater (86,000 kg water released at ~ 150 km)

(Block 2) Apollo BP (Boiler Plate), Apollo BP + Pegasus

Retired

Saturn 1B
Engines:
1. 8 ×  H-1 | S-I
2. 1 ×  J-2 | S-IVB

Total mass: 589,770 kg
Payload (LEO): 18,600 kg

Fairing:

(4)
(5)
(6)

  SA 201, 202. 205-210
  SA 203
  SA 204

Launches: 9 (Failures: 0)
/1966-1975/

Payload: Apollo CSM, Apollo LM (LEM), Apollo SLM, Apollo CSM + ASTP-DM

(CSM)

AJ10-137
R-4D × 16

(LM)

LMAE (ascent stage)
LMDE (descent stage)
R-4D × 8

Retired

Saturn 1B

Saturn V (3 stages)
Engines:
1. 5 ×  F-1 | S-IC
2. 5 ×  J-2 | S-II
3. 1 ×  J-2 | S-IVB

Total mass: 3,038,500 kg

Payload:

(LEO)
(TLT)

118,000 kg
47,000 kg

(185 km

Fairing:
(4)

Launches: 12 (Failures: 0)
/1967-1972/

Payload:
Apollo CSM + LTA
Apollo CSM + LTA B
Apollo CSM + LM

(CSM)

AJ10-137
R-4D × 16

(LM)

LMAE (ascent stage)
LMDE (descent stage)
R-4D × 8

Retired

Saturn V (3 stages)

Saturn V (2 stages)
Engines:
1. 5 ×  F-1 | S-IC
2. 5 ×  J-2 | S-II

Total mass:
3,038,500 kg

Payload:

(LEO)

75,000 kg (500 km)

Fairing:
(7)

Launches: 1 (Failures: 0)
/1973/

Payload: Skylab

Retired

Saturn V (2 stages)

Saturn I Centaur

Engines:
1. 8 ×  H-1 | S-I
2. 6 × RL-10  | S-4
3. 2 × RL-10  | Centaur

Saturn I - Dyna Soar

Never flown

Saturn 1B-A

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:

(LEO)

18,600 kg (185 km)

Saturn 1B-B

Engines:
1. 8 ×  H-1 | S-I
2. 1 ×  HG-3  | MS-IVB-2 (+)

Total mass: 652,440 kg

Payload:

(LEO)

22,700 kg (185 km)

Saturn 1B-C (INT-14)

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:

(LEO)

20,400 kg (185 km)

Status: Study /1965/

Saturn 1B-D

Engines:
0. 4 ×  UA1205
1. 8 ×  H-1 | S-I
2. 1 ×  J-2  | S-IVB

Total mass: 1,511,980 kg

Payload:

(LEO)

33,000 kg (185 km)

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:

(LEO)

33,000 kg (185 km)

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:

(LEO)

48,000 kg (185 km)

Status: Study /1966/

Never flown

Saturn INT- 05A

Engines:
1. 4 ×  FL
2. 1 ×  J-2  | S-IVB

Total mass: 1,818,800 kg

Payload:

(LEO)

43,034 kg (185 km)

Status: Study /1965/

Saturn INT - 15

Engines:
1. 4 ×  UA1205
2. 1 ×  J-2  | S-IVB

Total mass: 990,000 kg

Payload:

(LEO)

26,000 kg (169 km)

Status: Study /1966/

Saturn INT - 16

Engines:
1. 5 ×  UA1207
2. 1 ×  J-2  | S-IVB

Total mass: 1,284,000 kg

Payload:

(LEO)

28,000 kg (185 km)

Status: Study /1966/

Never flown

Saturn MLV-V 1

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:

(LEO)
(TLT)

137,250 kg
49,600 kg

(185 km)

Status: Study /1965/

Saturn MLV-V 1A

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:

(LEO)
(TLT)

145,000 kg
54,400 kg

(185 km)

Status: Study /1965/

Saturn MLV-V 2

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:

(LEO)
(TLT)

137,250 kg
53,550 kg

(185 km)

Status: Study /1965/

Saturn MLV-V 3

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:

(LEO)
(TLT)

160,400 kg
65,800 kg

(185 km)

Status: Study /1965/

Saturn MLV-V 4(S)

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:

(LEO)
(TLT)

118,000 kg
52,900 kg

(185 km)

Status: Study /1965/

Saturn MLV-V 4(S)-A

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:

(LEO)
(TLT)

160,880 kg
57,500 kg

(185 km)

Status: Study /1965/

Saturn MLV-V 4(S)-B

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:

(LEO)
(TLT)

171,990 kg
63,160 kg

(185 km)

Status: Study /1967/

Never flown

Saturn ELV

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:

(LEO)
(TLT)

200,000 kg
67,000 kg

(185 km)

Status: Study /1966/

Never flown

RETIRED

Missiles    Early Rockets    Delta    Atlas    Titan    Solid Launchers
Saturn    Space Shuttle    Delta 4    Atlas 3, 5    Vulcan    Falcon    Misc ...
Blue Origin Rockets    Starship    SLS    Unflown