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Rocket Engine, Liquid Fuel, Nike-Ajax

Air and Space Museum

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International media Interoperability Framework
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Object Details

Manufacturer

Aerojet General Corp.

Summary

This liquid propellant rocket engine of the Nike-Ajax, built by the Aerojet General Corporatoin, is the U.S.'s first operational surface-to-air missile. The missile used a solid propellant booster and liquid propellant second stage. The liquid sustainer engine produced 2,600 pounds of thrust for about 20 seconds. It used red fuming nitric acid and JP-4, a type of jet fuel, as its propellants. It was a very simple system with no moving parts for ease in operation and high reliability.
The propellants were forced into the combustion chamber by compressed air. Development of the engine was begun in late 1945 by Aerojet-General and the missile became operational in 1953 and remained in service until 1963. This object was donated to the Smithsonian in 1968 by the Aerojet General Corp.

Credit Line

Gift of Aerojet General Corp.

Inventory Number

A19680547000

Restrictions & Rights

Usage conditions apply

Type

PROPULSION-Rocket Engines

Materials

Stainless steel; aluminum caps on two inlet lines; black inside of nozzle, probably a ceramic, heat-resistant liner.

Dimensions

Overall: 8 3/4 in. wide x 1 ft. 10 in. long x 6 1/2 in. diameter, 22 lb. (22.23 x 55.88 x 16.51cm, 10kg)

Country of Origin

United States of America

See more items in

National Air and Space Museum Collection

Location

Steven F. Udvar-Hazy Center in Chantilly, VA

Exhibit Station

Rockets & Missiles

Data Source

National Air and Space Museum

Metadata Usage

Not determined

Link to Original Record

http://n2t.net/ark:/65665/nv9a0c6543b-f371-4226-8906-660a6fecbc82

Record ID

nasm_A19680547000

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Rockets and Missiles

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Rockets and Missiles

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