Products

HQ200WP Engine

Configuration

Single Shaft Compact Structure Design
1-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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