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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.
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The J-2 liquid propellant rocket engine, using liquid hydrogen and liquid oxygen, was the powerplant for the second and third stages of the Saturn V launch vehicle that took astronauts to the Moon in the Apollo program. The engine shown here was an early developmental model and produced 200,000 pounds of vacuum thrust. It made three tests for a total duration firing time of 291 seconds.
The Saturn V's second stage used a cluster of five J-2s, while the third stage had one J-2 that was gimballed, or steerable, so that this stage could be steered on its way to the Moon. The J-2 was developed and built by the Rocketddyne Division of the Rockwell International Corporation. NASA transferred this J-2 engine to the Smithsonian in 1970.
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
Date
1964
Country of Origin
United States of America
Type
PROPULSION-Rocket Engines
Manufacturer
Rocketdyne Division, Rockwell International Dimensions
Overall: 11 ft. × 6 ft. 8 3/8 in., 5740lb. (335.3 × 204.2cm, 2603.6kg)
3-D (Dimensions on stand): 365.8 × 205.7 × 243.8cm (12 ft. × 6 ft. 9 in. × 8 ft.) Materials
Stainless steel and other metals. Inventory Number
A19700261000
Credit Line
Transferred 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.