.jpg "MS400P Small-size turbofan engine © Konstantinos Panitsidis")
Photos from the personal collection of Konstantinos Panitsidis
Technical specifications 
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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 | - |
