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IIIF provides researchers rich metadata and image viewing options for comparison of works across cultural heritage collections.
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https://iiif.si.eduView ManifestView in Mirador ViewerUsage Conditions May ApplyUsage Conditions ApplyThere are restrictions for re-using this media. For more information, visit the Smithsonian's Terms of Use page.
IIIF provides researchers rich metadata and image viewing options for comparison of works across cultural heritage collections.
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https://iiif.si.eduView ManifestView in Mirador ViewerUsage Conditions May ApplyUsage Conditions ApplyThere are restrictions for re-using this media. For more information, visit the Smithsonian's Terms of Use page.
IIIF provides researchers rich metadata and image viewing options for comparison of works across cultural heritage collections.
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https://iiif.si.eduView ManifestView in Mirador ViewerUsage Conditions May ApplyUsage Conditions ApplyThere are restrictions for re-using this media. For more information, visit the Smithsonian's Terms of Use page.
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Shown here is the fuel injector head for the engine that lifted the ascent stage of the lunar excursion module (LEM) off the surface of the moon. Once aloft, the LEM docked with the orbiting command module and returned to Earth. This simple, light-weight engine produced a maximum thrust of 3,500 pounds and burned hypergolic (self-igniting) propellants.
NASA awarded the contract for the engine to the Bell Aerosystems Company in January 1963. Early on, Bell engineers struggled with combustion instability problems, prompting a redesign of the injector. The Rocketdyne Division of North American Aviation developed the replacement injector, which Bell incorporated into the engine shown here. NASA used this version in all of the Apollo lunar missions.
Transferred from NASA.
Display Status
This object is not on display at the National Air and Space Museum. It is either on loan or in storage.
Object Details
Country of Origin
United States of America
Type
PROPULSION-Components (Engine Parts)
Manufacturer
Rocketdyne Division, Rockwell International Dimensions
Overall (Injector Head): 11in. x 2 1/8in. (27.94 x 5.4cm)
Overall (Cover): 11 1/2in. x 6 1/2in. (29.21 x 16.51cm) Materials
Aluminum, Ink Inventory Number
A19731212000
Credit Line
Transferred to the National Air and Space Museum from the National Aeronautics and Space Administration
Data Source
National Air and Space Museum
Restrictions & Rights
Usage conditions apply
For more information, visit the Smithsonians Terms of Use.