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Rocket Motor, Solid Fuel, X-259

Air and Space Museum

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    Object Details

    Manufacturer

    Alleghany Ballistics Laboratory, Hercules Incorporated

    Summary

    This is the X-259, or Antares II, the third-stage, solid-fuel rocket motor for the all-solid fuel U.S. Scout launch vehicle. Antares II produced about 23,500 pounds of thrust. Like the other stages of the Scout, Antares was named after a star constellation. (The Scout's first, second, and fourth stages were the Algol, Castor, and Altair, respectively.)
    The Scout was conceived in 1958 as a low-cost launch vehicle for light payloads. The first Scout was launched in 1960 and continued as a very successful vehicle. This object was donated to the Smithsonian in 1968 by the Alleghany Ballistic Laboratory.

    Credit Line

    Gift of Alleghany Ballistics Laboratory

    Date

    ca. 1968

    Inventory Number

    A19680240000

    Restrictions & Rights

    Usage conditions apply

    Type

    PROPULSION-Rocket Engines

    Materials

    Filament-wound, resin-bonded glass fiber body with asbestos-filled SBR rubber. Windings by circumferential wraps of glass fiber coated with catalyzed epoxy resin. Aluminum nozzle fixture rings. Aluminum skirt rings bolted underneath forward dome.

    Dimensions

    Overall: 2 ft. 4 in. wide x 9 ft. 6 1/2 in. long x 2 ft. 5 in. diameter, 200 lb. (71.12 x 290.83 x 73.66cm, 90.7kg)

    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/nv9dcdd5bec-4512-48f7-a200-f22742537dd2

    Record ID

    nasm_A19680240000

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