HQ900G Engine
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
Characteristics
| Take-off Thrust kgf | 990 |
|
Take-off SFC kg/(kgf.h)
|
0.38 |
|
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 |
Applications
Business Jet /High altitude long endurance UAVs
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