HQ400WP Engine
Configuration
Single shaft compact structure design
3-stage Axial Compressor+Toroidal DC Combustion Chamber+1-stage Axial Flow Turbine+Simple Convergence Nozzle
Characteristics
| Take-off Thrust kgf | 450 |
|
Take-off SFC kg/(kgf.h)
|
1.22 |
| Total Pressure Ratio | 4.2 |
| Turbine Inlet Temp K(℃) | 1223(950) |
| Start Time s | 21 |
|
Power Supply kw/Volt
|
5.0/28.5 |
| Start Altitude m | 0-2000 |
Applications
High performance target drones / UAVs
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