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Pump, Liquid Propellant, Rocket Motor, R.H. Goddard, ca. 1924

National Air and Space Museum

Object Details

Manufacturer
Dr. Robert H. Goddard
Summary
This is probably a pump part made by the American rocket experimenter Robert H. Goddard (1882-1945) about 1924. These pump experiments were carried out before Goddard had flown any rockets. His early pumps operated by the evaporation of liquid oxygen, although he had not yet fully developed his liquid-propellant motors using liquid oxygen and gasoline. However, as he recorded in his notes, these early "experiments with small pumps clearly demonstrated that a very small piston pump for liquid oxygen is very impracticable. The larger pump operated satisfactorily…." But following this period, Goddard switched course and designed and built a rocket without any pumps at all. He used a very simple but practical pressure-fed propellant feed system, also using, in part, the evaporation of liquid oxygen.
In 1959, Goddard’s widow gave this pump part to the Smithsonian as part of a large collection of artifacts.
Credit Line
Gift of Mrs. Robert H. Goddard
Inventory Number
A19590089000
Restrictions & Rights
Usage conditions apply
Type
PROPULSION-Accessories (to an Engine)
Materials
Copper Alloy
Steel
Dimensions
3-D: 21 × 3.8 × 3.8cm (8 1/4 × 1 1/2 × 1 1/2 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_A19590089000
Metadata Usage (text)
Not determined
GUID (Link to Original Record)
http://n2t.net/ark:/65665/nv94aa6c38f-815d-42ee-8080-31a5c541c046

Related Content

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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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