Products

HQ600WS Engine

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


Characteristics

Take-off Thrust kgf 680
Take-off SFC kg/(kgf.h)
0.5
Bypass Ratio 2.15
Total Pressure Ratio 11.0
Turbine Inlet Temp K(℃)
1313(1040)
Dry Weight kg 135
Size(diameter/length) mm
472/1450


Applications

High altitude long endurance UAVs



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