200kg Thrust Turbojet Engine WF200WP
SKU: MD-P00291·Spare Parts & Components·Made to Order
Overview
Single shaft compact structure design 1-stage Centrifugal Compressor+ Toroidal DC Combustion Chamber+1-stage Turbine High performance target drones / UAVs Take-off SFC kg/(kgf.h)：1.12 Turbine Inlet Temp K( C)：1223(950) Size(diameter/length)(mm): 305/650
Technical specification
Specifications. Key specifications: 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.
Technical specification — 1 groups
Key specifications: 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.
Technical specifications
Specifications
- 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
Compatible aircraft
This part fits the following platforms.
Fitment data pending — contact us with your aircraft model.