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.
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{{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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