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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.[3] 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.
General characteristics
Capacity: 30 passengers ( under the AP-29 airworthiness regulations )
Length: 19.70 m
Rotor diameter: 21.10 m
Height: 5.13 m
Disc area: 349.5 m²
Empty weight: 8,300 kg
MTOW: 14,200 kg
Powerplant: 2 × Klimov TV7-117V or Pratt & Whitney Canada PW127/TS turboshaft, 1,864 kW (2,800 shp) each
Performance
Maximum speed: 320 km/h (at 500 m)
Range: 920 km with main tanks full
Service ceiling: 3,100 m (static) 8,300 m (dynamic) (21,320 ft)
Rate of climb: 9.2 m/s (1 811 ft/min)
Disc loading: 41 kg/m² (8.3 lb/ft²)
Power/mass: 260 W/kg (0.16 hp/lb)
[video=youtube_share;71KyigGkka0]http://youtu.be/71KyigGkka0[/video]
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.
General characteristics
Capacity: 30 passengers ( under the AP-29 airworthiness regulations )
Length: 19.70 m
Rotor diameter: 21.10 m
Height: 5.13 m
Disc area: 349.5 m²
Empty weight: 8,300 kg
MTOW: 14,200 kg
Powerplant: 2 × Klimov TV7-117V or Pratt & Whitney Canada PW127/TS turboshaft, 1,864 kW (2,800 shp) each
Performance
Maximum speed: 320 km/h (at 500 m)
Range: 920 km with main tanks full
Service ceiling: 3,100 m (static) 8,300 m (dynamic) (21,320 ft)
Rate of climb: 9.2 m/s (1 811 ft/min)
Disc loading: 41 kg/m² (8.3 lb/ft²)
Power/mass: 260 W/kg (0.16 hp/lb)
[video=youtube_share;71KyigGkka0]http://youtu.be/71KyigGkka0[/video]
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