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Data from Bayerl and the manufacturer General characteristics Crew: one Capacity: one passenger Length: 4.78 m (15 ft 8 in) Width: 1.73 m (5 ft 8 in) Height: 2.74 m (9 ft 0 in) Airfoil: NACA 8-H-12 Empty weight: 265 kg (584 lb) Gross weight: 450 kg (992 lb) Fuel capacity: 86 litres (19 imp gal; 23 US gal) Powerplant: 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke aircraft ...
An autogyro (from Greek αὐτός and γύρος, "self-turning"), or gyroplane, ... Open-frame aircraft are restricted to a minimum speed of 30 mph (48 km/h; 26 kn ...
Data from Bumble Bee Performance and Stress Analysis General characteristics Crew: 1 Length: 10 ft (3.0 m) Height: 7 ft 6 in (2.29 m) Empty weight: 213 lb (97 kg) Gross weight: 500 lb (227 kg) Powerplant: 1 × Rotax 447 2-cylinder air-cooled 2-stroke in-line piston engine, 40 hp (30 kW) Main rotor diameter: 23 ft (7.0 m) Propellers: 2-bladed fixed-pitch propeller Performance Maximum speed: 49 ...
The Monarch was designed to comply with the US Experimental - Amateur-built rules. It features a single main rotor, a single-seat open cockpit without a windshield, tricycle landing gear with wheel pants and a twin cylinder, liquid-cooled, two-stroke, dual-ignition 64 hp (48 kW) Rotax 582 engine in pusher configuration.
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The aircraft has a standard empty weight of 247 lb (112 kg). It features a single main rotor, a single-seat open cockpit without a windshield, tricycle landing gear and a twin-cylinder, air-cooled, two-stroke, dual-ignition 45 hp (34 kW) Zanzottera MZ 201 engine in pusher configuration. [1]
The Avian Gyroplane which is the inspiration for ARC's designs. In 2023, ARC Aerosystems acquired the intellectual property, all rights and type certification of the Avian Gyroplane (also called the "Pegasus" which had previously obtained FAA certification), including the last remaining flying example. [3]
The B-8's design is extremely minimalist, with not much more to the aircraft than a pilot's seat, a single tailfin, a rotor, and (in powered versions) the powerplant. In May 1968 a B-8 and B-8M were studied by the USAF under the Discretionary Descent Vehicle (DDV) program as the X-25B and X-25A respectively.