Configuration
Single shaft compact structure design
3-stage Axial Compressor + Toroidal DC Combustion Chamber+1-stage Axial Flow Turbine + simple convergence Nozzle
Applications
High performance target drones / UAVs
Characteristics
Take-off Thrust（ kgf ）：455
Take-off SFC kg/(kgf.h)：1.15
Total Pressure Ratio：4.2
Turbine Inlet Temp K(°C)：1223(950)
Dry Weight ( kg): 65.0
Size(diameter/length)(mm): 330/1250
