Object Details
Manufacturer
Aerojet General Corp.
Physical Description
Cylinder with nozzle affixed at rear; overall, glossy white with black stenciling; black nozzle; and aqua blue plastic rim on end; comes with separate cannister for igniter
Summary
This is the solid fuel rocket motor for the Sparrow II air-to-air missile. Produced by the Aerojet-General Corporation, the motor generated 7,800 pounds of thrust for 1.8 seconds, hence its designation 1.8KS7800. The same motor was also used in the Sparrow I and other members of the Sparrow missile family.
The U.S. Navy transferred the Sparrow II to the Smithsonian in 1958.
Credit Line
Transferred from U.S. Navy
Date
1957
Inventory Number
A19590099003
Restrictions & Rights
Usage conditions apply
Type
ARMAMENT-Missiles
Materials
Steel
Dimensions
Overall: 4ft 3 1/2in. x 8in. (130.81 x 20.32cm)
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_A19590099003