(Mil) Mi-38 @·AIRCRAFTUBE

  • Mil Mi-38-2 at the 2013 MAKS Airshow (Ramenskoye Airport, Russia) Mil Mi-38-2 at the 2013 MAKS Airshow (Ramenskoye Airport, Russia)
    Mil Mi-38-2 at the 2013 MAKS Airshow (Ramenskoye Airport, Russia)
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    Mi-38 (MAKS 2005)
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    Mi-382
  • Mi-382 (MAKS 2011) Mi-382 (MAKS 2011)
    Mi-382 (MAKS 2011)
  • Mi-38 (MAKS 2005) Mi-38 (MAKS 2005)
    Mi-38 (MAKS 2005)
  • Mil Mi-38-2 Mil Mi-38-2
    Mil Mi-38-2
  • Mi-38 Mi-38
    Mi-38
  • Mil Mi-38-2 at the MAKS-2013 Mil Mi-38-2 at the MAKS-2013
    Mil Mi-38-2 at the MAKS-2013
  • Mi-38 (MAKS-2005) Mi-38 (MAKS-2005)
    Mi-38 (MAKS-2005)
  • MAKS-2011 MAKS-2011
    MAKS-2011

Mil Mi-38

The Mil Mi-38 is a transport helicopter designed by Mil Moscow Helicopter Plant. 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 and was certified on 30 December 2015.

Design and development

The manufacturer plans to provide the Mi-38 with a new Tranzas "glass cockpit" avionics system and new composite main rotor blades. The helicopter is offered with a choice of either Klimov TV7-117V or Pratt & Whitney Canada PW127/TS turboshaft engines. The second prototype, powered by the PW127TS, made its first flight in December 2010. In 2013, the third prototype has been assembled at the Kazan Helicopter Plant.

The Mil Mi-38 prototypes have already set five records in the E1h class. The second prototype aircraft set an altitude record by reaching 8,620 meters (28,280 feet) without a payload. The second and third records were for climbing speed; the Mi-38 reached a height of 3,000 meters (9,843 feet) in six minutes, then followed this to reach 6,000 meters (19,685 feet) in 10 minutes and 52 seconds. Two further records were altitude records: the first was set at 7,895 meters (25,902 feet) with a 1,000-kg (2,205-lb) payload, the second at 7,020 meters (23,031 feet) with a 2,000-kg (4,409-lb) payload.

On 30 December 2015, Rosaviatsiya certified the Mi-38, completing the testing and certification program and allowing for the delivery of the first production model. Certification was based on the third and fourth flight-test prototypes with 2,500 shp Klimov TV7-117V engines.

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This text is available under the Creative Commons Attribution-ShareAlike License
Source : Article Mil Mi-38 of Wikipedia ( authors )

Specifications (Mi-38)

  • Crew : 1-2.
  • Capacity : .
    • 30 passengers (under the AP-29 airworthiness regulations).
    • Internal 6,000 kg (13,000 lb).
    • External 7,000 kg (15,000 lb).
  • Length : 19.70 m (64.6 ft).
  • Height : 5.13 m (16.8 ft).
  • Rotor diameter : 21.10 m (69.2 ft).
  • Disc area : 349.5 m² (3,762 sq ft).
  • Disc loading : 41 kg/m² (8.4 lb/sq ft).
  • Empty weight : 8,300 kg (18,300 lb).
  • Loaded weight : 14,200 kg (31,300 lb).
  • Max. takeoff weight : 16,200 kg (35,700 lb).
  • Maximum speed : 320 km/h (200 mph; 170 kn).
  • Cruise speed : 290 km/h (180 mph; 160 kn).
  • Range : 920 km (570 mi; 500 nmi) with main tanks.
  • Ferry range : 1,550 km (960 mi; 840 nmi) with an extra fuel tank.
  • Service ceiling : 5,900 m (19,400 ft) operational, 3,750 m (12,300 ft) hover.
  • Rate of climb : 9.2 m/s (1,810 ft/min).
  • Powerplant : Two Klimov TV7-117V or Pratt & Whitney Canada PW127/TS turboshaft.
  • Power : 2,800 shp (2,100 kW) each.
  • Power/mass : 296 W/kg (0.180 hp/lb).

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This text is available under the Creative Commons Attribution-ShareAlike License
Source : Article Mil Mi-38 of Wikipedia ( authors )
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