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
Next：HQ900G Engine
