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HELICOPTER VV-2

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VV-2 a high-speed, single-engine, two seat (tandem) helicopter. It is designed for either piloted or unmanned flight.
 

8020

8500

2200

Main Rotor - Composite Structure      Tail Rotor - Composite Structure      Diameter Tail Rotor 1.4 m

Landing Gear Tread 2 m.     Cabin Dimentions / Volume 0,73x1,2x2,02 m. / 1.7m3

 
 
 

PBS Czech Republic

TS 100 ZA 

Power

190 H.P. / 140 kW (Cruise)

245 H.P. / 180 kW (Take off-5minutes)

Fuel Flow                           Jet A, A1, B, TS-1, T2, RT

Fuel Tank Capacity                                           230 L

Fuel consumption                                   0,5 kg/kW/h

CREW
 
1 pilot and 1 passenger
Never Exceed Speed 252 km/h 
Maximum Cruise Speed 240 km/h | Long Range Cruise Speed 220 km/h | Rate of Climb 9 m/s
Range at LRC Speed 500 km
OGE Hover Ceiling 3400 m. | IGE Hover Ceiling 4000 m.
Max Take-off Weight 1100 kg
Empty Weight 565 kg | Max Gross Weight (External load) 900 kg. Useful Load (Internal) 380 kg.
 

HELICOPTER CAN BE UNMANNED

 

VV-2 is equipped with modern navigation instrumentation, including autopilot. This fact allows to access necessary information in any time.

 The possibility for installation of any equipment on customer’s desire. The precise analysis of every element of control panel, even location and luminance of signal indicators, will be carried for these purposes. This provides pilot with the most significant information, not diverting him from the flight.

Flight Deck

and 

Avionics