High Altitude Aircraft Turbofan Engine HQ900G For Long Endurance UAVs

Configuration
Low-pressure part: 1-stage Fan +Planetary Gear Reducer+2-stage IPC+2-stage LPT
Core part: 1-stage Centrifugal HPC+ Annular reflux combustion chamber+1-stage HPT
Exhaust: Separate exhaust, simply converge nozzle
 
Applications
Business Jet/High altitude long endurance UAVs
 
Characteristics
Take-off Thrust (kgf):991
Cruising SFC kg/( kgf.h): 0.68
Bypass Ratio: 5.7
Total Pressure Ratio: 15.1
Turbine Inlet Temp K(℃): 1311(1038)
Dry Weight (kg): 215
Size(diameter/length) (mm): 600/1400