Rocket Engine, Liquid Fuel, H-1
The H-1 liquid-fuel rocket engine was the first stage power plant for the Saturn 1 and Saturn 1B launch vehicles, the precursors to the Saturn V which took men to the Moon in the Apollo program. The Saturn 1 and Saturn 1B were each fitted with eight H-1 engines in their first stages. The engine uses RP-1 (kerosene) and liquid oxygen for this model's 188,000 pounds of thrust.
The H-1 was evolved directly from Army Ballistic Missile Agency projects, specifically the Jupiter and Juno V. With the approval of the Apollo Project, the Juno V was re-designated the Saturn. The successful launches of the Saturn 1 and Saturn 1B led the way to the Saturn V. The Saturn 1, with its eight H-1's, first flew on October 27, 1961, while the last Saturn 1B was flown on July 15, 1975, for the Apollo-Soyuz Test Project.
NASA transferred this H-1 engine to the Smithsonian Institution in 1980.
Transferred from the National Aeronautics and Space Administration
- Country of Origin
- United States of America
- ca. 1958-1975
- PROPULSION-Rocket Engines
- Chamber and nozzle coolant passages 347 stainless steel. Propellant tanks, lines, and valves, stainless steel. Pumps, aluminum alloys; turbine, Hastealloy. Injector, OHFC copper and 347 stainless steel.
- Combustion chamber made of 292 stainless steel tubes. The assembly, except for inlet manifold, was furnaced brazed with gold brazing alloy. Injectors, furnaced brazed.
- Overall: 100 in. long x 47 in. diameter (254 x 119.38cm)