Photos from the personal collection of Konstantinos Panitsidis


 Technical specifications      Photos      Video

 

 

Designers: Motor Sich, JSC Zaporozhye, Ukraine
Manufacturer: Motor Sich, JSC Zaporozhye, Ukraine

The MS400P engine is designed for installation in light aircraft, as well as UAVs and tactical cruise missiles.

 


TECHNICAL SPECIFICATIONS

Fuel -
Oil -
Max power rating (H=0, M=0, ISA) 400 kgf (3,92 kN)
Specific fuel consumption  ≤ 0,85 (8,66 kN) kg/kgf*h
Max thrust, cruise power  -
Specific fuel consumption, cruise power  -
Pressure ratio, take-off power rating  -
Bypass ratio -
Temperature of the gas at the turbine intake, take-off power rating -
Air flow rate, take-off power rating -
Compressor rotation frequency low-pressure, take-off power rating -
Compressor rotation frequency high-pressure, take-off power rating
Diameter 320 mm
Height 455 mm
Width -
Length 875 mm
Weight 85 kg
Specified service life -

 


PHOTOS  MS400P