Thrust Specific Fuel Consumption - Typical Values of SFC For Thrust Engines

Typical Values of SFC For Thrust Engines

Specific fuel consumption (SFC), specific impulse, and effective exhaust velocity numbers for various rocket and jet engines.
Engine type Scenario SFC in lb/(lbf·h) SFC in g/(kN·s) Specific impulse (s) Effective exhaust velocity (m/s)
NK-33 rocket engine Vacuum 10.9 309 331 3,240
SSME rocket engine Space shuttle vacuum 7.95 225 453 4,423
Ramjet Mach 1 4.5 127 800 7,877
J-58 turbojet SR-71 at Mach 3.2 (Wet) 1.9 53.8 1,900 18,587
Rolls-Royce/Snecma Olympus 593 Concorde Mach 2 cruise (Dry) 1.195 33.8 3,012 29,553
CF6-80C2B1F turbofan Boeing 747-400 cruise 0.605 17.1 5,950 58,400
General Electric CF6 turbofan Sea level 0.307 8.696 11,700 115,000


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