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A coaxial-rotor aircraft is an aircraft whose rotors are mounted one above the other on concentric shafts, with the same axis of rotation, but turning in opposite directions (contra-rotating). This rotor configuration is a feature of helicopters produced by the Russian Kamov helicopter design bureau .
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The VA115 features dual, coaxial main rotors with NACA 23012 airfoils, a single-seat open cockpit without a windshield, tricycle landing gear and a two-cylinder, air-cooled, two stroke, fuel-injected 50 hp (37 kW) Hirth F23 engine. [1] The aircraft fuselage is made from metal tubing, with a small cockpit fairing. Its dual two-bladed rotors each ...
Hiller Aircraft Company is an American private aerospace company, based in Firebaugh, California. It was founded in 1942 as Hiller Industries by Stanley Hiller to develop helicopters. History
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The aircraft fuselage is made from welded steel tubing. Its dual two-bladed rotors have diameters of 14.5 ft (4.4 m) and incorporate dual flapping hinges. Directional control is achieved by tilting the rotor mast. The aircraft has an empty weight of 500 lb (227 kg) and a gross weight of 850 lb (386 kg), giving a useful load of 350 lb (159 kg).