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Liquid Oxygen Pump, Rocket Engine, R.H. Goddard

National Air and Space Museum

Object Details

Manufacturer
Dr. Robert H. Goddard
Summary
This appears to be a part of one of the first rocket pumps tested by the American rocket pioneer Dr. Robert H. Goddard in 1923 for his first experiments with liquid propellant rocket motors. It is a one-way vale with a piston. However, it was only used in ground tests.
Goddard used liquid oxygen and kerosene to test his first pumps, although he preferred liquid oxygen and gasoline as his standard propellants. This object was donated to the Smithsonian by Mrs. R. H. Goddard in 1959.
Credit Line
Gift of Mrs. Robert H. Goddard
Inventory Number
A19590086000
Restrictions & Rights
Usage conditions apply
Type
PROPULSION-Components (Engine Parts)
Materials
Steel
Brass
Dimensions
3-D: 23.5 × 1cm (9 1/4 × 3/8 in.)
Country of Origin
United States of America
See more items in
National Air and Space Museum Collection
National Air and Space Museum
Record ID
nasm_A19590086000
Metadata Usage (text)
Not determined
GUID (Link to Original Record)
http://n2t.net/ark:/65665/nv9e13750ae-8ddd-4462-a6ee-4ffdac63751a

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    Air and Space Museum
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International media Interoperability Framework
IIIF provides researchers rich metadata and media viewing options for comparison of works across cultural heritage collections. Visit the IIIF page to learn more.
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