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Saturn A-1
Rocket
Rocket
| Field | Value | |
|---|---|---|
| name | Saturn A-1 | |
| country-origin | United States | |
| function | Uncrewed launch vehicle | |
| manufacturer | Von Braun | |
| height | 49.62 m | |
| alt-height | 162.29 ft | |
| diameter | 6.52 m | |
| alt-diameter | 21.39 ft | |
| mass | 524,484 kg | |
| stages | 3 (all used on various vehicles, now retired) | |
| status | Never flown | |
| sites | N/A | |
| capacities | for LEO | |
| stage1name | S-I | |
| stage1engines | 8 H-1 | |
| stage1thrust | 7,582 kN | |
| stage1time | 150 seconds | |
| stage1fuel | RP-1/LOX | |
| stage2name | Titan I | |
| stage2engines | 2 LR-87-3 | |
| stage2thrust | 1,467 kN | |
| stage2time | 138 seconds | |
| stage2fuel | RP-1/LOX | |
| stage3name | Centaur C | |
| stage3engines | 2 RL-10A-1 | |
| stage3thrust | 133 kN | |
| stage3time | 430 seconds | |
| stage3fuel | LH2 / LOX | |
| image | [[File:Saturn B, 1959.jpg | 100px]] |
|country-origin = United States |alt-height = 162.29 ft |alt-diameter = 21.39 ft
Saturn A-1, studied in 1959, was projected to be the first version of Saturn I and was to be used if necessary before the S-IV liquid hydrogen second stage became available.
It was designed as a three stage vehicle. The S-I first stage (initially proposed for the Juno V rocket and eventually used on Saturn I) would propel the Saturn A-1 into space, continuing the flight with a Titan I missile based second stage. Finally a Centaur C high-energy double-engine third stage could send a payload into its final Earth orbit or to other planets.
The Saturn A-1 never flew, but all proposed stages were used on different launch vehicles. Today, they are all retired.
References
References
- (2016-11-14). "Saturn A-1".
- Bilstein, Roger E.. (1996). "Stages to Saturn: a technological history of the Apollo/Saturn launch vehicles". National Aeronautics and Space Administration, NASA History Office : For sale by the U.S. G.P.O., Supt. of Docs.
- (October 1, 1959). "Lunar Exploration with Saturn-Boosted Systems". [[Army Ballistic Missile Agency]].
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