This is a partly graphite experimental liquid propellant rocket motor thrust chamber and nozzle developed in the 1960s or 70s by Reaction Motors, Inc. The graphite was chosen to help absorb the heat of combustion of the motor. It was used for short firing periods and for tests only. The motor was donated by Reaction Motors to the Smithsonian Institution in 1977.
Display Status
This object is not on display at the National Air and Space Museum. It is either on loan or in storage.
Object Details
Country of Origin
United States of America
Type
PROPULSION-Components (Engine Parts)
Manufacturer
Reaction Motors, Inc.
Dimensions
Overall: 12 in. long x 8 in. diameter (30.5 x 20.3cm)
Materials
Partly made of graphite, with metal rings inserted at both ends.
Inventory Number
A19771261000
Credit Line
Gift of Thiokol Chemical Corporation
Data Source
National Air and Space Museum
Restrictions & Rights
Usage conditions apply
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