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Rocket Motor, Liquid Fuel, HWK 109-509 A-1

Air and Space Museum

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    Object Details

    Manufacturer

    Helmuth Walter KG

    Summary

    The 109-509A-1 was the power plant for the World War II German Me 163 B-1 Komet rocket fighter. It was the first variable-thrust rocket engine to be installed in a service aircraft and employed hydrogen peroxide with a hydrazine hydrate/methanol mixture as propellants. Some peroxide was diverted to a catalytic chamber containing potassium permanganate, producing steam to drive turbopumps to move the propellants The engine produced from 200-1800 kg (660-3740 lbs) thrust for 8-10 minutes. Developed by the firm of Helmut Walter in Kiel, it went into series production in August 1944. The Me 163 B-1, the world's first and only operational rocket fighter, was used in attacks against U.S. bombers in the fall of 1944, but did not prove very successful.
    The Smithsonian received this engine as a gift from Purdue University in 1967, which presumably had received it from the U.S. Air Force after World War II.

    Credit Line

    Gift of Purdue University School of Mechanical Engineering

    Date

    1944-1945

    Inventory Number

    A19680002000

    Restrictions & Rights

    Usage conditions apply

    Type

    PROPULSION-Rocket Engines

    Materials

    Steel, Stainless Steel, Aluminum, Paint

    Dimensions

    Overall: 2 ft. 3 in. tall x 3 ft. 1/2 in. wide x 8 ft. 5 1/2 in. deep x 8 in. diameter, 365 lb. (68.6 x 92.7 x 257.8 x 20.32cm, 165.6kg)

    Country of Origin

    Germany

    See more items in

    National Air and Space Museum Collection

    Location

    Steven F. Udvar-Hazy Center in Chantilly, VA

    Exhibit Station

    World War II Aviation

    Data Source

    National Air and Space Museum

    Metadata Usage

    Not determined

    Link to Original Record

    http://n2t.net/ark:/65665/nv9579ecd2d-55b3-499b-a04c-9be99958bdc6

    Record ID

    nasm_A19680002000

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    Rockets and Missiles

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