Developed in the 1950s, the S-3 D Jupiter engine powered the U.S.'s first intermediate range (1600 miles) ballistic missile (IRBM). A modification of the Redstone engine, the Jupiter engine, which operated on liquid oxygen and RP-1 (a type of kerosene), produced 150,000 lbs of thrust for 178 seconds. The Jupiter missile itself was 58 feet (17.7 m) long, 8.75 feet (2.7 m) in diameter, and weighed 110,000 lbs (49,900 kg).
NASA transferred this engine to the Museum in 1969.
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
Date
1958
Country of Origin
United States of America
Type
PROPULSION-Rocket Engines
Manufacturer
Rocketdyne Division, Rockwell International
Dimensions
3-D (Approximate): 398.8 × 190.5 × 205.7cm (13 ft. 1 in. × 6 ft. 3 in. × 6 ft. 9 in.)
Materials
HAZ MAT: Asbestos
HAZ MAT: Thoriated Magnesium
Ferrous Alloy
Aluminum Alloy
Rubber
Copper Alloy
Electrical Wiring
Inventory Number
A19700262000
Credit Line
Transferred from the National Aeronautics and Space Administration
Data Source
National Air and Space Museum
Restrictions & Rights
Usage conditions apply
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