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TRDD MS-400 engine designed for subsonic unmanned aerial vehicles of different purpose and cruise missiles.. will be manufactured as a part of the Grom 2 missile system.. the cruise missile part of it..
Main advantages of the engine:
Maximum power SLS, ISA Thrust, kgf (kN) 400 (3,92) SFC, kg/kgf•h (kg/kN•h)max ≤ 0.85 (86.6) Overall dimensions Engine diameter with respect to cowling, mm 315 Length, mm 850 Dry weight, kg 85
Main advantages of the engine:
- high reliability;
- high fuel efficiency;
- low thrust-to-weight ratio;
- long period of operation and storage in aircraft and insignificant scope of maintenance operations;
- quick and reliable starting within wide range of environmental conditions as well as altitudes and airspeed;
- resistance to instability of engine inlet air pressure and temperature;
- capability of inadvertent surge recovery;
- compact and simple single-shaft design;
- built-in electric generator providing power supply to aircraft systems;
- electronic-and-hydraulic automatic control system which does not need adjustment during storage and operation;
- feasibility of air bleeds for aircraft needs.
Maximum power SLS, ISA Thrust, kgf (kN) 400 (3,92) SFC, kg/kgf•h (kg/kN•h)max ≤ 0.85 (86.6) Overall dimensions Engine diameter with respect to cowling, mm 315 Length, mm 850 Dry weight, kg 85
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