200kg Thrust Turbojet Engine HQ200WP

Configuration
Single shaft compact structure design
1-stage Centrifugal Compressor+ Toroidal DC Combustion Chamber+1-stage Turbine

Applications
High performance target drones / UAVs

Characteristics
Take-off Thrust（kgf）：220
Take-off SFC kg/(kgf.h)：1.12
Total Pressure Ratio：3.8
Turbine Inlet Temp K(°C)：1223(950)
Dry Weight( kg): 34.0
Size(diameter/length)(mm): 305/650