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2 x Klimov TV7-117V or PW127TS turboshaft, 1,864 kW (2,500 shp) each. The Mil Mi-38 is a helicopter designed by Mil. Originally intended as a replacement for the Mil Mi-8 and the Mi-17, it is being marketed in both military and civil versions. It flew for the first time on 22 December 2003.
Mi-38 zaprezentował zdolność wykonywania zawisu bez wpływu ziemi z masą 16 350 kg oraz pułap statyczny 3 100 metrów z masą startową 14 200 kg. Do maja 2008 roku pierwszy prototyp wylatał około 100 godzin, a w 2010 roku dalsze próby przerwano, do tego czasu pierwszy prototyp wykonał 84 loty.
4 cze 2024 · The Mi-38 is also fitted with modified main rotor blades and a new Tranzas "glass cockpit" avionics system. The Mi-38 will be fitted out with up-to-date integrated avionics. Five multifunctional color displays will screen flight data.
The Mi-38 is powered by two Pratt & Whitney Canada / Russia PW127TS turboshaft engines, rated at 2,500hp (1,864kW), fitted with FADEC (full authority digital engine control). The twin engines are installed above the main cabin.
Find out how to recognise all the different versions of the Mil Mi-38, and learn what are the differences between the Mi-38 and similar aircraft types like the Leonardo (AgustaWestland) AW101 (EH101), Sikorsky S-92, Sikorsky S-61R/CH-3 and Mil Mi-8/Mi-17 family.
Mi-38 responds to a conventional helicopter layout featuring a six-bladed main rotor and a tail rotor both leverage the Mi-28 design implemented by MIL. Its airframe also incorporates composites and modular architecture allowing for faster maintenance compared to Mi-8 and Mi-17 helicopters.
Initial versions of the twin-engined aircraft wielded either the BK-2500 or PW-127T/V engines. Maximum internal and slung loads are 6000 kg and 7000 kg, repectively; passenger capacity is 32 or 16 stretchers.
