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Flow Indicator, Liquid Oxygen, Rocket Engine, R.H. Goddard

Air and Space Museum

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    Object Details

    Manufacturer

    Dr. Robert H. Goddard

    Summary

    This is a flow regulator for liquid oxygen, also called a lox [flow] indicator, and was used by Robert H. Goddard for some of his earliest liquid fuel rocket experiments, about 1923-1924.
    Mrs. Robert H. Goddard donated this object to the Smithsonian Institution in 1959 as part of a large collection of artifacts from her husband.

    Credit Line

    Gift of Mrs. Robert H. Goddard

    Inventory Number

    A19590080000

    Restrictions & Rights

    Usage conditions apply

    Type

    EQUIPMENT-Test

    Materials

    Steel, Brass, Felt, Copper, Natural Fabric, Cardboard, Plastic

    Dimensions

    3-D: 41.9 x 6.7 x 30.5cm (16 1/2 x 2 5/8 x 12 in.)

    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/nv96e4f5075-57e1-4003-8d7c-abd70661f18f

    Record ID

    nasm_A19590080000

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    Rockets and Missiles

    Image of F-1 rocket engine cluster on display

    Rockets and Missiles

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