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Rocket Engine, Liquid Fuel, XLR-11

Air and Space Museum

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International media Interoperability Framework
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    Object Details

    Manufacturer

    Reaction Motors, Inc.

    Summary

    This is the XLR-11, also called the 6000C-4, one of the most widely used U.S. liquid-propellant rocket engines that powered the Bell X-1 and other rocket research aircraft. Developed by Reaction Motors, Inc. in 1945, it produced a maximum thrust of 6,000 pounds from its four combustion chambers. The engine's most famous application was powering the X-1, the first plane to reach the speed of sound on 14 October 1947.
    It was also used in the X-1A, X-1B, X-1D, X-1E, Douglas D-558-1 Skyrocket, and XF-91. Two tandem 6000C-4's served as the Interim Engine for the X-15 from 1960-1961, and it also powered several NASA Lifting Bodies (the HL-10, MS-F3, X-24A, and X-24B). This object was donated to the Smithsonian in 1952 by Reaction Motors, Inc.

    Credit Line

    Reaction Motors, Inc.

    Date

    ca. 1945-1953

    Inventory Number

    A19530051000

    Restrictions & Rights

    Usage conditions apply

    Type

    PROPULSION-Rocket Engines

    Materials

    Overall Steel, Adhesive, Synthetic Fabric, Stainless Fabric, Copper, Aluminum, Paint, Stainless Steel, Brass

    Dimensions

    Overall: 24 × 56 1/2 in., 210lb. (61 × 143.5cm, 95.3kg)
    Storage (Artex Crate): 91.4 × 177.8 × 91.4cm (36 × 70 × 36 in.)
    Approximate (Weighed with Stand): 182.3kg (402lb.)

    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/nv9529de4b4-e917-4117-94ce-3df02b2f4621

    Record ID

    nasm_A19530051000

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