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Home Aerospace & Aeronautics Light Multi-Purpose 5-Seated Helicopter Of The Category With 2 Internal Combustion Turbines (ICT)

Light Multi-Purpose 5-Seated Helicopter Of The Category With 2 Internal Combustion Turbines (ICT)


The main aircraft performance characteristics of the helicopter:

  • Maximal takeoff weight ---------------------------------- 1400 kg
  • Weight of empty helicopter ------------------------------ 750 kg
  • Maximal airspeed ---------------------------------------- 220 km/h
  • Cruising speed (for maximum range) ---------------------- 180 km/h
  • Economical speed (for maximum time of flight) ------------100 km/h
  • Fuel consumption per 1 km ------------------------------- 0,28 kg/km
  • Fuel consumption per 1 hour ----------------------------- 33 kg/h
  • Maximum range ability ----------------------------------- 600 km
  • Maximum flight endurance -------------------------------- 5 h
  • Static altitude ----------------------------------------- 2500 m
  • Dynamic altitude ---------------------------------------- 5000 m
  • Crow ---------------------------------------------------- 1 man (90 kg)
  • Maximum seating capacity -------------------------------- 4 men.(4х90kg)
  • Commercial cargo weight in cargo variant of helicopter -- 380 kg
  • Length of helicopter with revolving screws ---------------11,45 m
  • Height of helicopter up to center of main rotor head -----2,72 m
  • Main rotor diameter --------------------------------------10,0 m
  • Antitorque propeller diameter ----------------------------1,6 m

Innovative Aspect and Main Advantages

The helicopter has 2 ICT (a new rotary engines) with power 180 h.p. which has weight of 42 kg of our own development. According to JAR-27, the helicopters with 2 engines are permitted to fly above built-up area. There are no such light helicopters at the world market, because all light helicopters have only one heavy piston engine now. The main advantages:

  • A light helicopter of the category A with a price of a light helicopter of the category B.
  • The possibility to fly above built-up area and take-off in urban zone.

Areas of Application

  • Use of light helicopters by municipal services: police, firemen, army, and so on.
  • For private and corporation purposes.
  • For active recreations and sports.

Stage of Development

Feasibility study.

Contact Details

Research and Development Enterprise “TechnoRe-source”, Ltd. “EURORESOURCE Corp.”
Drachko Eugene F., PhD, director
3. Krasnoarmeysky line, Kiev, 03680, Ukraine.
Tel. /fax: +38 044/ 490-37-47.
E-mail: This e-mail address is being protected from spambots. You need JavaScript enabled to view it

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