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Rocket Engine, Liquid Fuel, Apollo Lunar Module Ascent Engine

Air and Space Museum

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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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    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

    Data Source

    National Air and Space Museum

    Metadata Usage

    Not determined

    Link to Original Record

    http://n2t.net/ark:/65665/nv9451e9808-9c7e-4cf9-bd3c-f18dcfc9574b

    Record ID

    nasm_A19721169000

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