Thrust-Specific Fuel Consumption
Calculate thrust-specific fuel consumption from fuel flow and thrust.
TSFC
0.24000 kg/(N h)
2.3536 lb/(lbf h)
Fuel flow
2,880.0 kg/h
0.800 kg/s
Calculation breakdown
Fuel-to-thrust ratio
TSFC is the fuel mass flow required to hold one unit of thrust for one unit of time.
2.354 lb/(lbf h)
SI hourly TSFC
0.24000 kg/(N h)
0.00006667 kg/(N s)
Imperial TSFC
2.3536 lb/(lbf h)
common jet-engine reporting unit
Fuel flow
0.800 kg/s
2,880.0 kg per hour
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