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Rocket Engine, Liquid Fuel, Cutaway, LR-79-NA-9 (Thor)

National Air and Space Museum

Object Details

Manufacturer
Rocketdyne Div., North American Rockwell
Summary
Shown here is the LR-79 (Model LR-79-NA-9) rocket engine for the U.S. Air Force's Thor intermediate range ballistic missile (IRBM). Development of the Thor began in 1955. The Air Force activated the first Thor batteries in England in 1959 and removed them from service four years later.
Developed and built by the Rocketdyne division of North American Aviation, the LR-79 incorporated a bell-shaped nozzle to improve the engine's overall efficiency. The propellant consisted of RP-1, a type of kerosene, and liquid oxygen. Rocketdyne developed two versions of the LR-79. The MB-1 and MB-3 produced 135,000 and 150,000 pounds of thrust respectively. The engine shown here is an MB-1, used for training purposes at Chanute Air Force Base, Illinois in 1960.
The U.S. Air Force transferred this engine to the Museum in 1965.
Credit Line
Transferred from the U.S. Air Force
1957-1958
Inventory Number
A19650277000
Restrictions & Rights
Usage conditions apply
Type
PROPULSION-Rocket Engines
Materials
Mainly stainless steel; pipes, aluminum; stand, steel
Dimensions
Overall: 8ft x 11ft 3/4in. x 5ft 6in., 2000lb. (243.84 x 337.11 x 167.64cm, 907.2kg)
Country of Origin
United States of America
See more items in
National Air and Space Museum Collection
National Air and Space Museum
Record ID
nasm_A19650277000
Metadata Usage (text)
Not determined
GUID (Link to Original Record)
http://n2t.net/ark:/65665/nv9214ddcd5-6b15-4b3e-b98f-5f55d8384a01

Related Content

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    Air and Space Museum
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