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The Saturn MLV rockets were actually a concept family of variants to be developed from the venerable Saturn V lunar rocket. The family is comprised of the MLV-V-1, MLV-V-1A, MLV-V-1/J-2T/200K, MLV-V-1/J-2T/250K, MLV-V-2, MLV-V-3, MLV-V-4(S), MLV-V-4(S)-A.
TABLE CAPTION
|
1st Stage |
2nd Stage |
3rd Stage |
LEO Payload |
MLV-V-1 |
MS-IC-1 |
MS-II |
MS-IVB |
137,250 kg |
MLV-V-1A |
MS-IC-1A |
MS-II-1A |
MS-IVB-1A |
145,000 kg |
MLV-V-1/J-2T/200K |
MS-IC-1 |
MS-II-1-J-2T/200K |
- |
- |
MLV-V-1/J-2T/250K |
MS-IC-1 |
MS-II-1-J-2T/250K |
- |
- |
MLV-V-2 |
MS-IC-1 |
MS-II-1 |
MS-IVB-2 |
137,250 kg |
MLV-V-3 |
MS-IC-1 |
MS-II-2 |
MS-IVB-2 |
160,440 kg |
MLV-V-4(S)* |
S-IC |
MS-II-4(S)B |
MS-IVB-1 |
118,000 kg |
MLV-V-4(S)-A* |
MS-IC-4(S)-B |
MS-II-1 |
MS-IVB-1 |
160,880 kg |
- Indicates zero stage strap on boosters. In both cases 4x-Titan UA-1205
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