Object Details
Manufacturer
Rocketdyne Division, Rockwell International (CA)
Summary
The H-1 liquid-fuel rocket engine was the first stage powerplant of the Saturn 1 and Saturn 1B launch vehicles, precursors to the Saturn V that 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 used RP-1 (kerosene) and liquid oxygen. The model shown here may be the second variation which produced 188,000 pounds of thrust. The Saturn 1 first flew in 1961 while the last Saturn 1B was flown in 1975 for the low-Earth orbit Apollo-Soyuz Test Project. This cutaway version of the engine was transferred to the Smithsonian in 1970 from the NASA Marshall Space Flight Center.
Credit Line
Transferred from the National Aeronautics and Space Administration
Date
ca. 1958-1969
Inventory Number
A19700285000
Restrictions & Rights
Usage conditions apply
Type
PROPULSION-Rocket Engines
Materials
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.
Dimensions
Overall: 8 ft. 4 in. long x 3 ft. 11 in. diameter (254 x 119.38cm)
Country of Origin
United States of America
See more items in
National Air and Space Museum Collection
Data Source
National Air and Space Museum
Link to Original Record
Record ID
nasm_A19700285000