Aircraft Turbofan Engine HQ600WS
INQUIRY
Configuration
Low-pressure part: 1-stage Fan+2-stage IPC+2-stage LPT
Core part: 1-stage Centrifugal HPC+ Annular reflux combustion chamber+1-stage HPT
Exhaust: Mixed exhaust, simply converge nozzle
Applications
High altitude long endurance UAVs
Characteristics
Take-off Thrust ( kgf): 700
Cruising SFC kg/(kgf.h):0.75
Bypass Ratio: 2.15
Total Pressure Ratio: 11.0
Turbine Inlet Temp K(°C)： 1313(1040)
Dry Weight（kg）：135
Size(diameter/length) （mm）: 472/1450
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