What types of Mi-17 helicopters are available?

The Mi-17 is a single-rotor medium utility helicopter with tail rotor designed by the Miri Moscow Helicopter Plant (formerly Miri Experimental Design Bureau). The Mi-17 was first displayed at the Paris Airshow in 1981 and exported to Cuba in 1983. Existing types: Mi-17P, electronic interference type; Mi-17VA, can be installed operating table and other medical equipment, carrying doctors and three nurses; Mi-17M/17V, equipped with TV3-117NV engine, optional nose radar, floating landing gear and firefighting equipment; Mi-17MD, the prototype was displayed at the Paris Airshow in 1995, and can carry 40 passengers.

The Mi-17 is fitted with 2 sets of Klimov TV3-117MT turboshaft engines, with a single power of 1434 kW. The rotor diameter is 21.29 meters, tail rotor diameter is 3.91 meters, length (rotor, tail rotor rotation) is 25.352 meters, height (to the top of the hub) is 4.755 meters. Empty weight (loaded equipment) 7100 kg, maximum payload (internal) 4000 kg, (external) 3000 kg, normal takeoff weight 11000 kg, maximum takeoff weight 13000 kg. Mi-17 maximum level flight speed (maximum takeoff weight) 250 km / h, maximum cruise speed (maximum takeoff weight) 240 km / h, the practical ceiling (normal takeoff weight) 50,000 meters, normal range 495 km.