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Rocket Engine, Liquid Fuel, Apollo Lunar Module Ascent Engine

National Air and Space Museum

Object Details

Manufacturer
Bell Aerosystems Company
Summary
This is a Lunar Module Ascent Engine (LMAE). The LMAE was part of the Lunar Module (LM), the spaecraft that landed Apollo astronauts on the moon. The LMAE was a curcial component of the spacecraft. It powered the LM ascent stage, carrying the astronauts off the surface of the moon and back to the Command Module spacecraft.
This engine was one of the test engines for the LMAE program. It was fired in 1964 at White Sands Test Facility, New Mexico for a total of 380 seconds. It was later used during LM thermal tests at Grumman Aerospace, which was the prime contractor for the LM.
This engine was donated to the Smithsonian in 1972 by the Grumman Aerospace Co.
Credit Line
Grumman Aerospace Corp.
Inventory Number
A19721169000
Restrictions & Rights
Usage conditions apply
Type
PROPULSION-Rocket Engines
Materials
Refrasil phenolic ablator, insulated with asbestos phenolic and glass fiber wrapped structural case; propellant lines, stainless steel; injector and valves, aluminum; Teflon seals in valves; valve housings, stainless steel
Dimensions
Overall: 2ft x 4ft 4 1/2in., 250lb. (61 x 133.4cm, 113.4kg)
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_A19721169000
Metadata Usage (text)
Not determined
GUID (Link to Original Record)
http://n2t.net/ark:/65665/nv9451e9808-9c7e-4cf9-bd3c-f18dcfc9574b

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There are restrictions for re-using this image. For more information, visit the Smithsonian's Terms of Use page .
International media Interoperability Framework
IIIF provides researchers rich metadata and media viewing options for comparison of works across cultural heritage collections. Visit the IIIF page to learn more.
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