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Rocket Engine, Liquid Fuel, Surveyor Vernier, also Designated TD-339

Air and Space Museum

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International media Interoperability Framework
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    Object Details

    Manufacturer

    Reaction Motors Div., Thiokol Chemical Corp.

    Summary

    This is a vernier rocket motor for the Surveyor unmanned lunar landing probe, America's first spacecraft to soft-land on the Moon. It provided small bursts of thrust for mid-course trajectory correction maneuvers and attitude and velocity control before and during the landing. It produced 30-104 pounds of thrust. For protection from solar radiation, exposed surfaces were coated with very thin gold plate.
    The Reaction Motors Division of the Thiokol Chemical Corporation developed the vernier which was first used operationally on Suveyor 1 that soft-landed on the Moon in 1966. Five Surveyors out of seven launched were successfully landed on the Moon up to 1968.
    The motor was donated to the Smithsonian by the Jet Propulsion Lab in 1970.

    Credit Line

    Transferred from the National Aeronautics and Space Administration

    Date

    ca. 1963-1968

    Inventory Number

    A19700233000

    Restrictions & Rights

    Usage conditions apply

    Type

    PROPULSION-Rocket Engines

    Materials

    Steel
    Plastic
    Aluminum
    Synthetic
    Inorganics
    Glass
    Copper Alloy
    Coating
    Unknown Metal
    Textile

    Dimensions

    3-D: 33.5 × 21.6 × 14cm, 2.9kg (1 ft. 1 3/16 in. × 8 1/2 in. × 5 1/2 in., 6.4lb.)

    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/nv9f97163ad-68b9-4d4a-8c39-074077972cb8

    Record ID

    nasm_A19700233000

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