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Shown here is the RL-10 rocket engine. Designed and built by the Pratt and Whitney Aircraft Division of the United Aircraft Corporation, the RL-10 was the world's first operational liquid hydrogen/liquid oxygen, restartable rocket engine. Two RL-10 engines, each capable of producing 15,000 pounds of thrust, powered the Centaur upper stage carried atop the Atlas and Titan launch vehicles. The National Aeronautics and Space Administration (NASA) launched the first Atlas-Centaur rocket in 1966, during which the RL-10 successfully demonstrated a full-thrust re-start in space.
A cluster of six RL-10 engines also powered the second stage of the Saturn I launch vehicle, predecessor of the giant Saturn V rocket that carried astronauts to the Moon between 1969 and 1972.
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-Rocket Engines
Manufacturer
Pratt & Whitney Dimensions
Overall: 27 9/16 in. tall x 70 in. long x 40 in. diameter (70 x 177.8 x 101.6cm) Materials
Chamber, 347 stainless steel brazed with silver; piping, polished stainless steel; pump, aluminum casting; heat exchanger, nickel alloy Inventory Number
A19940100000
Credit Line
Transferred from the National Aeronautics and Space Administration
Data Source
National Air and Space Museum
Restrictions & Rights
Usage conditions apply
For more information, visit the Smithsonians Terms of Use.
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