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Desing, computation and manufacture of hybrid UAV

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M

metalist93

Member
Joined
Jul 13, 2016
Messages
15
Location
Kharkov
Hello everybody

I'm Alex and I aircraft engineer. Me pleasantly to share experience and knowledge of Desing, computation and manufacture UAV.

Technical feature
​
  1. Maximum Takeoff weight - 10 kg
  2. Payload - 2 kg
  3. Fuel - 2 kg (piston engine version)
  4. Power of engine - 2.5hp (piston engine version)
  5. Power of engine - 2.05 kW (electro engine version)
  6. Propeller speed - 9000 rpm
  7. Max speed - 120 km/h
  8. Min speed - 50 km/h
  9. Flight time - over 120 minute (piston engine version)
  10. Cruising altitude - up to 2000 m
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All questions you can send to my email: [email protected]
or write here
 
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