.jpg "MS400P Small-size turbofan engine © Konstantinos Panitsidis")
In numbers Through the lens 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
| DESIGNER | Motor Sich, JSC Zaporozhye |
| COUNTRY | Ukraine |
| TYPE |
Small-size turbofan engine
|
| Installed On (aerial means) |
Small aircraft, UAVs, cruise missiles.
|
| Fuel | - |
| Oil | - |
| Max power rating (H=0, M=0, ISA) | 400 kgf (3,92 kN) |
| Specific fuel consumption | ≤ 0,85 (86,6 kN) kg/kgf*h |
| Maximum 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 | - |
| OVERALL DIMENSIONS | |
| Diameter | 320 mm |
| Height | 455 mm |
| Width | - |
| Length | 875 mm |
| WEIGHT | |
| Engine weight | 85 kg |
| Specified service life | - |
Photos MS400P
