Rocket Engine Turbo Pump, Cutaway, F-1

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Display Status:

This object is not on display at the National Air and Space Museum. It is either on loan or in storage.

Collection Item Summary:

This pump was used on the F-1 liquid fuel rocket engine, the powerplant for the first stage of the Saturn V launch vehicle that took the first astronauts to the Moon for six successful landing missions from 1969 to 1972 in the Project Apollo program. The F-1 produced 1.5 million pounds of thrust.

The first stage was fitted with five F-1's for a total lift-off thrust of 7.5 million pounds. The F-1 used RP-1, a type of kerosene, and liquid oxygen as the propellants. The F-1's 2,500 pound turbopump pumped in the propellants at 42,500 gallons per minute. This pump was donated to the Smithsonian in 1975 by the NASA Marshall Space Flight Center.

Collection Item Long Description:

Data Source

National Air and Space Museum

Restrictions & Rights

Do not reproduce without permission from the Smithsonian Institution, National Air and Space Museum

Credit Line

Transferred from the National Aeronautics and Space Administration

Materials

Inlets, volutes, and impellers, aluminum alloy casting. Turbine wheels and manifold assemblies, nickel alloy.

Dimensions

Overall: 5 ft. 2 in. tall x 4 ft. wide, 2000 lb. (w/Crate 2,500lb.) (157.48 x 121.92cm, 907.2kg)

Country of Origin

United States of America

Type

PROPULSION-Components (Engine Parts)

Inventory Number

A19751580000

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