80kg Thrust Turbojet Engine NM-80
SKU: MD-P00471·Spare Parts & Components·Made to Order
Overview
Nm-80wp turbojet engine is a turbojet engine composed of a single stage centrifugal compressor and an axial flow turbine, which has strong anti-overload and distortion ability. It has three starting modes: motor driven rotation, air blowing and gunpowder impact. At present, it is used in large mobile target aircraft, and can be used in missile power after improvement. Technical parameter for 80kg Thrust Turbojet Engine Type: centrifugal compressor, axial turbine Dimensions: 230mm x 670mm Fuel consumption rate: ≯1.6kg/(daN.h) Maximum use height: 9000m Operating temperature: -40 C~55 C
Technical specification
Specifications. Key specifications: Type centrifugal compressor, axial turbine, Dimensions 230mm x 670mm, Body weight ≯ 13kg, Maximum thrust ≮80daN, Fuel consumption rate ≯1.6kg/(daN.h), Maximum use height 9000m, Maximum use speed 0.8Ma, Anti-overload 6g, Operating temperature -40 C~55 C, Working life ≮20h.
Technical specification — 1 groups
Key specifications: Type centrifugal compressor, axial turbine, Dimensions 230mm x 670mm, Body weight ≯ 13kg, Maximum thrust ≮80daN, Fuel consumption rate ≯1.6kg/(daN.h), Maximum use height 9000m, Maximum use speed 0.8Ma, Anti-overload 6g, Operating temperature -40 C~55 C, Working life ≮20h.
Technical specifications
Specifications
- Type
- centrifugal compressor, axial turbine
- Dimensions
- 230mm x 670mm
- Body weight
- ≯ 13kg
- Maximum thrust
- ≮80daN
- Fuel consumption rate
- ≯1.6kg/(daN.h)
- Maximum use height
- 9000m
- Maximum use speed
- 0.8Ma
- Anti-overload
- 6g
- Operating temperature
- -40 C~55 C
- Working life
- ≮20h
Compatible aircraft
This part fits the following platforms.
Fitment data pending — contact us with your aircraft model.