Saturn V S-IVB cutaway.jpg
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Summary
| Description |
English: This cutaway drawing shows the S-IVB (third stage) of the Saturn V launch vehicle. As a part of the Marshall Space Flight Center’s (MSFC) “building block” approach to the Saturn development, the S-IVB stage was utilized in the Saturn IB launch vehicle as a second stage and, later, the Saturn V launch vehicle as a third stage. The 59 foot long and 22 feet diameter stage was powered by a single J-2 engine, initially capable of 200,000 pounds of thrust. |
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| Source | https://images.nasa.gov/details-0600309 (image link) |
| Author | NASA/MSFC |
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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: MSFC-0600309. 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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This image or video was catalogued by Marshall Space Flight Center of the United States National Aeronautics and Space Administration (NASA) under Photo ID: MSFC-67-IND-1200-66. 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 | 15:01, 22 March 2020 | | 3,000 × 2,119 (5.73 MB) | wikimediacommons>Huntster | {{Information |Description={{en|1=This cutaway drawing shows the S-IVB (third stage) of the Saturn V launch vehicle. As a part of the Marshall Space Flight Center’s (MSFC) “building block” approach to the Saturn development, the S-IVB stage was utilized in the Saturn IB launch vehicle as a second stage and, later, the Saturn V launch vehicle as a third stage. The 59 foot long and 22 feet diameter stage was powered by a single J-2 engine, initially capable of 200,000 pounds of thrust.}} |Sourc... |
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