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Rocket Engine, Liquid Fuel, Apollo Lunar Module Descent Engine

Air and Space Museum

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International media Interoperability Framework
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    Object Details

    Manufacturer

    Bell Aerospace Company

    Summary

    This is the liquid propellant Lunar Module Ascent Engine. It was one of the most important in the manned Project Apollo missions since it was used to lift up the ascent stage of the Lunar Excursion Module (LEM) from the surface of the Moon which was then to dock with the Command Module (CM) orbiting the Moon. In the event of a too fast approach to the Moon, the engine could also be used to slow down the descent. It produced 3,500 pounds of thrust. The engine was developed and made by the Bell Aerospace Company. This engine was transferred to the Smithsonian from the NASA Marshall Space Flight Center in 1975.

    Credit Line

    Transferred from NASA/Marshall Space Flight Center

    Inventory Number

    A19751447000

    Restrictions & Rights

    Usage conditions apply

    Type

    PROPULSION-Rocket Engines

    Materials

    Probably phenolic nozzle; metal propellant valves and inlets

    Dimensions

    Height, 92 inches; diameter, maximum, at base, 59 inches

    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/nv943567cf2-4775-4112-8d05-23eadaf50618

    Record ID

    nasm_A19751447000

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