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Rocketdyne F-1

Rocket engine
The F-1, commonly known as Rocketdyne F-1, is a rocket engine developed by Rocketdyne. This engine uses a gas-generator cycle developed in the United States in the late 1950s and was used in the Saturn V rocket in the 1960s and early 1970s. Wikipedia
Engine price: $15 million
Chamber pressure: 70 bars (1,015 psi; 7 MPa)
Cycle: Gas-generator (Open Cycle)
Length: 18.5 feet (5.6 m)
Manufacturer: Rocketdyne
Mass flow: 3,945 lb/s (1,789 kg/s) (LOX); 1,738 lb/s (788 kg/s) (RP-1)
Mixture ratio: 2.27 (69% O2, 31% RP-1)