चित्र:RL-10 rocket engine.jpg

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विवरण
English: RL-10 engine characteristics. The RL-10 engine was developed under the management of the Marshall Space Flight Center (MSFC) to power the Saturn I upper stage (S-IV stage). The six RL-10 engines, which used liquid hydrogen and liquid oxygen as propellants, were arranged in a circle on the aft end of the S-IV stage.
दिनांक circa १९६०
date QS:P,+1960-00-00T00:00:00Z/9,P1480,Q5727902
स्रोत https://images.nasa.gov/details/9801769; originally at http://mix.msfc.nasa.gov/ABSTRACTS/MSFC-9801769.html
लेखक NASA/Marshall Space Flight Center
This image or video was catalogued by Marshall Space Flight Center of the United States National Aeronautics and Space Administration (NASA) under Photo ID: 9801769.

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Public domain 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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The original description page was here. All following user names refer to en.wikipedia.
  • 2004-06-10 04:21 Reubenbarton 640×480× (81533 bytes) RL-10 high energy rocket engine

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