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This wing provides docile handling and ease of rigging. Standard empty weight of 247 lb (112 kg) when equipped with the Rotax 447 engine. [1] [3] [4] [5] XP Racer Racer carriage equipped with the XP11 racing wing, giving a 75 mph (121 km/h) cruise speed. Standard empty weight of 271 lb (123 kg) when equipped with the Rotax 503 engine. [3] [4] [5]
It has a span of 9.55 m (31.3 ft) span wing, a nose angle of 130°, an aspect ratio of 6.0:1 and uses an "A" frame weight-shift control bar. Like the similar Air Creation BioniX wing, the NuviX incorporates a unique "corset" system that allows the pilot to adjust the wing's trailing edge geometry in flight to optimize performance.
An ultralight trike or paratrike is a type of powered hang glider where flight control is by weight-shift. [1] These aircraft have a fabric flex-wing from which is suspended a tricycle fuselage pod driven by a pusher propeller. The pod accommodates either a solo pilot, or a pilot and a single passenger.
Typical wings used have a 9.5 to 10.2 m (31.2 to 33.5 ft) span wing, are supported by a single tube-type kingpost and use an "A" frame weight-shift control bar. The standard powerplant is the twin cylinder, air-cooled, two-stroke , dual-ignition 64 hp (48 kW) Rotax 582 engine.
The Ascender III-A is similar to the original Pterodactyl Pfledge. It lacks a canard and pitch control is by weight shift, although it incorporates some refinements, such as nose wheel steering. The 2003 price was USD$6800. [1] [2] [13] DFE Ascender III-B
The Jazz was designed to comply with the Fédération Aéronautique Internationale microlight category, including the category's maximum gross weight of 450 kg (992 lb). ). It features a cable-braced hang glider-style high-wing, weight-shift controls, a two-seats-in-tandem open cockpit with a cockpit fairing, tricycle landing gear with wheel pants and a single engine in pusher configurat
Data from Bertrand and P&M Aviation General characteristics Crew: one pilot Capacity: one passenger (100kg pilot and passenger weight capacity) x Wingspan: 10.4 m (34 ft 1 in) Wing area: 15.6 m 2 (168 sq ft) Empty weight: 204 kg (450 lb) Gross weight: 409 kg (902 lb) Fuel capacity: 49 litres (11 imp gal; 13 US gal) Powerplant: 1 × Rotax 912UL four cylinder, four-stroke aircraft engine, 60 kW ...
Its 10.60 m (34.8 ft) span wing is supported by a single tube-type kingpost and uses an "A" frame weight-shift control bar. The powerplant is a twin cylinder, air-cooled, two-stroke , dual-ignition 50 hp (37 kW) Rotax 503 or the liquid-cooled 64 hp (48 kW) Rotax 582 engine.