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