Vortech Kestrel Jet
The Vortech Kestrel Jet is an American tip-jet helicopter that was designed in the 1980s. Kits for amateur construction were originally provided by Vortech and plans remain available.[1][2][3][4] Design and developmentThe aircraft was designed to fit into the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 254 lb (115 kg). The aircraft has a standard empty weight of 175 lb (79 kg). It features a single main rotor, a single-seat open cockpit without a windshield and skid landing gear. Power is supplied by two G8-2-20 rotor tip jets that run on propane, consuming 12 U.S. gallons (45 L; 10.0 imp gal) per hour and producing 47 lb (21 kg) of thrust each.[1][2][4] The aircraft fuselage is made from bolted-together aluminum tubing. Its main rotor is 24 ft (7.3 m) in diameter. Due to the lack of torque produced there is no tail rotor and instead the Kestrel mounts a circular-shaped rudder for directional control. Controls consist only of cyclic, rudder and throttle.[1][2] Specifications (Kestrel Jet)Data from Cliche, Vortech and KitPlanes[1][2][3] General characteristics
Performance
Avionics
References
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