File:S-IV rocket stage.jpg
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S-IV_rocket_stage.jpg (640 × 480 pixels, file size: 82 KB, MIME type: image/jpeg)
Summary
<a href="https://en.wikipedia.org/wiki/Saturn_S-IV" class="extiw" title="w:Saturn S-IV">S-IV Saturn I</a> rocket second stage. "This cutaway of the Saturn I S-IV stage (second stage) illustrates the booster's components. Powered by six RL-10 engines, the S-IV stage was capable of producing 90,000 pounds of thrust. Development of the Saturn S-IV stage by the Marshall Space Flight Center (MSFC) contributed many technological breakthroughs vital to the success of the Apollo lunar program, including the use of liquid hydrogen as a propellant. " NASA
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File history
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 23:44, 3 January 2017 | | 640 × 480 (82 KB) | 127.0.0.1 (talk) | <a href="https://en.wikipedia.org/wiki/Saturn_S-IV" class="extiw" title="w:Saturn S-IV">S-IV Saturn I</a> rocket second stage. "This cutaway of the Saturn I S-IV stage (second stage) illustrates the booster's components. Powered by six RL-10 engines, the S-IV stage was capable of producing 90,000 pounds of thrust. Development of the Saturn S-IV stage by the Marshall Space Flight Center (MSFC) contributed many technological breakthroughs vital to the success of the Apollo lunar program, including the use of liquid hydrogen as a propellant. " NASA |
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