File:Second Stage for SA-9.jpg
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Summary
| Description |
English: The Saturn I S-IV stage (second stage) assembly for the SA-9 mission underwent the weight and balance test in the hanger building at Cape Canaveral. The S-IV stage had six RL-10 engines which used liquid hydrogen and liquid oxygen as its propellants arranged in a circle. Each RL-10 engine produced a thrust of 15,000 pounds, a total combined thrust of 90,000 pounds. The SA-9 mission was the first Saturn with operational payload Pegasus I, meteoroid detection satellite, and launched on February 16, 1965.
Deutsch: Die zweite Stufe einer Saturn I (SA-9). |
| Date | Taken on 1 November 1964 |
| Source | http://mix.msfc.nasa.gov/abstracts.php?p=1506 (image link) |
| Author | NASA/MSFC |
| Permission (Reusing this file) |
http://mix.msfc.nasa.gov/copyright.html |
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This image or video was catalogued by Marshall Space Flight Center of the United States National Aeronautics and Space Administration (NASA) under Photo ID: 6416600. This tag does not indicate the copyright status of the attached work. A normal copyright tag is still required. See Commons:Licensing. Other languages:
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Licensing
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This file is in the public domain in the United States because it was solely created by NASA. NASA copyright policy states that "NASA material is not protected by copyright unless noted". (See Template:PD-USGov, NASA copyright policy page or JPL Image Use Policy.) |  |
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 09:33, 20 October 2010 | | 3,000 × 2,369 (5.38 MB) | Uwe W. | == Summary == {{Information |Description={{en|1=The second Stage for a Saturn I rocket. (SA-9) Orginal relase to the photo: The Saturn I S-IV stage (second stage) assembly for the SA-9 mission underwent the weight and balance test in the hanger buildin |
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