Saturn A-1
![]() | |
| Function | Uncrewed launch vehicle |
|---|---|
| Manufacturer | Von Braun |
| Country of origin | United States |
| Size | |
| Height | 49.62 m (162.29 ft) |
| Diameter | 6.52 m (21.39 ft) |
| Mass | 524,484 kg |
| Stages | 3 (all used on various vehicles, now retired) |
| Capacity | |
| Payload to low Earth orbit | |
| Mass | 13,600 kg (30,000 lb) |
| for LEO | |
| Launch history | |
| Status | Never flown |
| Launch sites | N/A |
| First stage - S-I | |
| Engines | 8 H-1 |
| Thrust | 7,582 kN |
| Burn time | 150 seconds |
| Propellant | RP-1/LOX |
| Second stage Titan I | |
| Engines | 2 LR-87-3 |
| Thrust | 1,467 kN |
| Burn time | 138 seconds |
| Propellant | RP-1/LOX |
| Third stage - Centaur C | |
| Engines | 2 RL-10A-1 |
| Thrust | 133 kN |
| Burn time | 430 seconds |
| Propellant | LH2 / LOX |
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.[1] It was proposed as a launcher for Project Horizon, a scientific / military base on the Moon project, at a time when the U.S. Department of the Army, Department of the Navy, and Department of the Air Force had total responsibility for U.S. space program plans.[2][3][4]
The rocket was designed as a three stage vehicle.[5] The S-I first stage (initially proposed for the Juno V rocket and eventually used on Saturn I) with eight H-1 engines would propel the Saturn A-1 into space, continuing the flight with a Titan I[6]: 3–6 missile based second stage with two LR-87-3 engines. Finally a Centaur[6]: 3–6 C high-energy double RL-10A-1 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.
See also
References
- ↑ "Saturn A-1". November 14, 2016. Archived from the original on November 14, 2016. Retrieved May 27, 2024.
- ↑ Ordway, Frederick I.; Sharpe, Mitchell R.; Wakeford, Ronald C. (October 1, 1988). "Project Horizon: An early study of a lunar outpost". Acta Astronautica. 17 (10): 1105–1121. Bibcode:1988AcAau..17.1105O. doi:10.1016/0094-5765(88)90194-4. ISSN 0094-5765.
- ↑ "Nearly 60 Years Ago, the U.S. Army Hatched a Plan to Put Soldiers on the Moon". Popular Mechanics. December 26, 2022. Retrieved December 16, 2023.
- ↑ "Horizon Lunar Outpost". www.astronautix.com. Retrieved December 16, 2023.
- ↑ Bilstein, Roger E. (1996). Stages to Saturn: a technological history of the Apollo/Saturn launch vehicles (PDF). The NASA history series. Washington, DC: National Aeronautics and Space Administration, NASA History Office : For sale by the U.S. G.P.O., Supt. of Docs. p. 49. ISBN 978-0-16-048909-9.
- 1 2 Lunar Exploration with Saturn-Boosted Systems (PDF) (Technical report). Army Ballistic Missile Agency. October 1, 1959. Archived (PDF) from the original on May 31, 2023. Retrieved May 31, 2023.
- Project Horizon Report: Volume I, Summary and Supporting Considerations (PDF). United States Army. June 9, 1959.
- Project Horizon Report: Volume II, Technical Considerations & Plans (PDF). United States Army. June 9, 1959.

