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The base model Profi wing is a cable-braced, king post-equipped hang glider-style wing for two-place trikes, while the Profi TL is a "topless" design, lacking the king post and using streamlined lower lift struts instead of wires. The topless design lowers the overall height of the wing and allows storage in lower-roofed hangars.
The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight category and the US light-sport aircraft rules. [2] [3] It features a strut-braced hang glider-style high-wing, weight-shift controls, a two-seats-in-tandem open cockpit, retractable wheeled tricycle landing gear and dual floats and a single engine in pusher configuration.
The BB Microlight BB-two seater is a Hungarian ultralight trike, designed and produced by BB Microlight of Baja, Hungary. The aircraft is supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft.
The trike carriage is of composite materials and is an aerodynamically faired design. Its 34.68 ft (10.6 m) span wing is supported by a single tube-type kingpost and uses an "A" frame weight-shift control bar.
North Wing Design is an American aircraft manufacturer, specializing in hang gliders, light-sport aircraft and ultralight trikes. The company was based in East Wenatchee, Washington and later moved to Chelan, Washington. [1] [2] [3] [4]
The wing is a cable-braced, king post-equipped hang glider-style wing designed as a high performance and competition wing for two-place trikes, although it is also used for flight training. It currently comes in one size, the iXess 15, named for its metric wing area of 15 m 2 (160 sq ft), although a 13 m 2 (140 sq ft) version was once available.
Data from Cliche and Purdy General characteristics Crew: one Capacity: one passenger Length: 2.1 m (7 ft) Wingspan: 10 m (33 ft) Wing area: 15.2 m 2 (164 sq ft) Empty weight: 136 kg (300 lb) Gross weight: 363 kg (800 lb) Fuel capacity: 53 litres (12 imp gal; 14 US gal) Powerplant: 1 × Rotax 503 twin cylinder, two-stroke, air-cooled aircraft engine Performance Maximum speed: 130 km/h (80 mph ...
Data from Cliche and Bertrand General characteristics Crew: one Wingspan: 32 ft 10 in (10 m) Wing area: 240 sq ft (22 m 2) Empty weight: 290 lb (132 kg) Gross weight: 660 lb (299 kg) Fuel capacity: 10 U.S. gallons (38 L; 8.3 imp gal) Powerplant: 1 × Rotax 447 twin-cylinder, two-stroke air-cooled aircraft engine, 40 hp (30 kW) Performance Cruise speed: 25 mph (40 km/h, 22 kn) Stall speed: 19 ...