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Rocket Engine, Liquid Fuel, A-7, Redstone Missile

Air and Space Museum

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International media Interoperability Framework
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Object Details

Manufacturer

Rocketdyne Div., North American Rockwell

Summary

The Redstone engine is one of the most historic developments in U.S. rocket technology. As the powerplant for the Redstone missile, it was this country's first large-scale operational rocket engine. It went on to power the Jupiter-C, a modification of the Redstone missile that placed the U.S.'s first artificial satellite, Explorer 1, in 1958. In 1961, another modified Redestone, the Mercury-Redstone 3, launched the first American into space, Alan B. Shepard. The thrust of the engine as used in the Redstone missile was 78,000 lbs. As modified for use as a booster for Shepard's Mercury spacecraft, it produced 83,000 lbs of thrust. The engine shown here appears to have been an earlier experimental model of the A-7 version. It was donated to the Smithsonian in 1970 by the Rocketdyne Division of North American Aviation, Inc.

Inventory Number

A19700252000

Restrictions & Rights

Usage conditions apply

Type

PROPULSION-Rocket Engines

Materials

Combustion chamber and injectors, 4130 steel; propellant lines, pumps, impellers, and valves, aluminum alloys.

Dimensions

Overall: 8 ft. 4 in. long x 2 ft. 9 in. diameter (254 x 83.82cm)

Country of Origin

United States of America

See more items in

National Air and Space Museum Collection

Data Source

National Air and Space Museum

Metadata Usage

Not determined

Link to Original Record

http://n2t.net/ark:/65665/nv90ad493b1-3584-4c10-9942-2259d4ee8ab2

Record ID

nasm_A19700252000

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