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DESCRIPTION
Single seat PAV (Personal Aerial Vehicle) VTOL (Vertical Take-Off and Landing) Foldable multicopter with tiltrotor Hybrid powerplant, full electric propulsion CLASSIFICATION Experimental Aircraft (FAA*) Electric Motorcycle CONTROLS Driving Wheel and Joystick, fly-by-wire electrical controls, drive-by-wire controls NAVIGATION Single integrated automotive and avionic controls TRANSFORMATION Full transformation into flight mode in less than 1 minute STRUCTURE Fuselage: Epoxy-impregnated carbon fiber, Acrylic Canopy Chassis: Epoxy-impregnated perforated steel LANDING SURFACES Concrete, Ashpalt, Grass, snow, ice SAFETY Triple-modular redundancy Occupant Restraint Systems – Load limiting seat belts, Airbags (optional) Fault-tolerant design 6 fixed propulsion units Ballistic parachute/Ejector seat (optional) |
OPERATING CONDITIONS
25 mph max wind (take-off and landing) -20 to 50 °C (-4 to 122 °F) temperature range Rain OPERATOR Up to 198 cm (6 ft 6 in) / 113 kg (250 lbs) SIZE 3 ft 6 in wide (with collapsed rotors) / 8 ft 6 in (with open rotors) 8 ft 6 in long 5 ft 4 in high Empty Weight 188 kg (414 lbs) FUEL Gasoline 20.8 l (5.5 gal) Battery 8.8 kWh CHARGING 120 V / 15 A 20% – 100% : 7.4 hrs 120 V / 20 A 20% – 100%: 5.5 hrs 240 V / 50 A 20% – 100%: 67 mins 240 V / 2×50 A 20% – 80%: 25 mins RANGE 96km (60 miles) (@Operator of 95 kg / 210 lb) STATIC THRUST 600kg (1,320 lbs) PERFORMANCE @Max Take-off Weight Cruise Speed 100km (62 mph) Max altitude 1524 m (5000 ft) Stall speed 0 mph Max. climb rate 1000 fpm Max. descent rate 1000 fpm |