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Sky Explorer VN-36


Regional Light aircraft S.T.O.L. "Sky Explorer VN-36" ("Vnedorozhnik  36") developed by Voronezh State Technical University. With the participation of Voronezh Aircraft Company "Sky Explorer VN-36" is designed to carry 15-19 passengers or an equivalent volume of cargo - 1800 kg. Able to take off and land on unprepared platform length from 110 meters. Up to 30% of the airframe components are made ​​of composite materials. Comfortable cabin for the crew (2 persons) and comfortable cabin for passengers, spacious cargo cabin. Possible alterations germosalona under various options - economy, luxury, sanitary, commercial (convertible fuselage). Automatic control system and balance in all modes of flight, including emergency situations. Support system "VN-36" includes two plans - the top and bottom with a positive influence on each other, as in cruising, and the take-off and landing mode.

 

  • Operating Temperature Range: - 50/40 
  • Maximum lateral wind velocity at  takeoff (landing): 15 m / s 
  • Operation with unprepared sites, strength of the soil, from 4.5 kg / cm ² 
  • Runway length (for take-off using any flat unprepared ground): 280 m
  • The minimum length of the runway-run (dry soil, concrete): 110 m 
  • Takeoff - mileage (high-altitude area, wet grass, wet soil, snow-covered lane): 150 m|
  • Fuel consumption, kg per passenger-kilometer: 0,020 
 

 

  • Maximal occupation, 19 passengers
  • Seat pitch, 0.80 m
  • Crew 2
  • Engine Type
  • Engine power, hp 2h 850
  • Screw diameter, 2.65
  • Take-off thrust, kgf 2h1600
  • Take-off weight, kg 7100
  • Curb weight, kg
  • The maximum weight of fuel, kg 1900
  • Maximum payload, kg 2500
  • Range with max. comm. load, km 1400
  • Range with max. fuel capacity, 3 100 km
  • Cruising speed, km / h 460
  • Most advantageous speed, km / h 405
  • Cruising altitude, 8.3 km
  • Runway length, m 230 *
  • Takeoff / run, m (concrete) 120
  • Interior type sealed
  • Dimensions Salon (length * height * width)
  • Weight engines total, 380 kg
  • The relative weight of engines (Gdv / Go) 0,05