400kg Thrust Turbojet Engine WF400WP
SKU: MD-P00290·Spare Parts & Components·Made to Order
Overview
Single shaft compact structure design 3-stage Axial Compressor + Toroidal DC Combustion Chamber+1-stage Axial Flow Turbine + simple convergence Nozzle High performance target drones / UAVs Take-off Thrust（ kgf ）：455 Take-off SFC kg/(kgf.h)：1.15 Turbine Inlet Temp K( C)：1223(950) Size(diameter/length)(mm): 330/1250
Technical specification
Specifications. Key specifications: 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.
Technical specification — 1 groups
Key specifications: 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.
Technical specifications
Specifications
- 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
Compatible aircraft
This part fits the following platforms.
Fitment data pending — contact us with your aircraft model.