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Rocketdyne

Apollo H-1

H-1
Engine statistics
Specification
Applications Saturn 1B first stage (8 clustered)
Propellants LOX/RP-1
Thrust at Sea Level 205,000 lb
Isp at sea level 263 s
Mixture Ratio 2.23:1
Weight 2009 lb
Chamber Pressure 700 psia
Area Ratio 8:1
Engine Cycle
Pump Design Pressures