Country of origin United States Application Booster Status Retired | Manufacturer Rocketdyne Successor H-1 Propellant LOX / RP-1 | |
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The Rocketdyne S-3D was an American liquid fueled rocket engine produced between 1956 and 1961 for use on the PGM-19 Jupiter and PGM-17 Thor missiles, and the Juno II rocket. Its design was later used as the basis for the H-1 rocket engine, also the Rolls-Royce RZ.2.
References
Rocketdyne S-3D Wikipedia(Text) CC BY-SA