File:RL-10 rocket engine.jpg

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Summary

Description
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.
Date circa 1960
date QS:P,+1960-00-00T00:00:00Z/9,P1480,Q5727902
Source https://images.nasa.gov/details/9801769; originally at http://mix.msfc.nasa.gov/ABSTRACTS/MSFC-9801769.html
Author 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.

This tag does not indicate the copyright status of the attached work. A normal copyright tag is still required. See Commons:Licensing.
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Licensing

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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Date/TimeThumbnailDimensionsUserComment
current14:52, 28 March 2020Thumbnail for version as of 14:52, 28 March 20201,024 × 768 (157 KB)HuntsterHigher resolution.
12:44, 25 June 2009Thumbnail for version as of 12:44, 25 June 2009640 × 480 (80 KB)Giovanni-P{{Information |Description={{en|RL-10 high energy rocket engine This picture was downloaded from NASA Marshall Spaceflight Center Image (MIX)) Exchange server: http://mix.msfc.nasa.gov/ABSTRACTS/MSFC-9801769.html}} |Source=Transferred from [http://en.wi
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