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Boeing Rocketdyne

RS-27A

RS-27A Engine
Engine statistics
Specification Main Vernier (x2)
Applications Delta II Roll control
Propellants LOX/RP-1
Thrust in Vaccum 237,000 lb
Thrust at Sea Level 200,000 lb 1,012 lb (x2)
Isp at sea level(s) 255
Isp at altitude 302
Mixture Ratio 2.245:1
Weight 2528 lb
Chamber Pressure 700 psia
Area Ratio 12:1
Engine Cycle ????
Pump Design Pressures ????