Saturn Apollo Program
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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Details
NASA ID
9801769
Date Created
January 1, 1960
Center
MSFC
Media Type
image
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