HQ200WP Engine
Configuration
Single Shaft Compact Structure Design1-stage Centrifugal Compressor+Toroidal DC Combustion Chamber+1-stage Turbine
Characteristics
Take-off Thrust
220
Take-off SFC kg/(kgf.h)
1.12
Total Pressure Ratio
3.8
Turbine Inlet Temp K(℃)
1223(950)
Start Time s
55
Power Supply kw/Volt
2.5/28.0
Start Altitude m
0-4500
Applications
High performance target drones / UAVs
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