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Medway Microlights factory, in Rochester, Kent. Medway Microlights is a British aircraft manufacturer, specializing in the manufacture of ultralight trikes and fixed wing microlight aircraft . The company is located in Rochester, Kent .
Apollo Ultralight Aircraft is a Hungarian aircraft manufacturer based in Eger.The company specializes in the design and manufacture of ultralight aircraft, gyroplanes and ultralight trikes, in the form of kits for amateur construction and ready-to-fly aircraft for the European Fédération Aéronautique Internationale microlight and the American light-sport aircraft categories.
The company's X-Air 'S' and 'F' models have been successful in the market and are exported widely. [4] The new Hawk model, known as Hanuman in India, is currently awaiting Indian and UK certification. [5] The ultralights manufactured by Raj Hamsa are some of the least expensive available in India and many parts of the world. [6]
Ultralight aviation (called microlight aviation in some countries) is the flying of lightweight, 1- or 2-seat fixed-wing aircraft. Some countries differentiate between weight-shift control and conventional three-axis control aircraft with ailerons , elevator and rudder , calling the former "microlight" and the latter "ultralight".
The Tiger Cub Developments (TCD) Sherwood Ranger is a single engine, tandem two seat biplane microlight designed and built in the United Kingdom in the early 1990s. Kits were originally produced by TCD; later, design rights were acquired by The Light Aircraft Company Ltd (TLAC) who resumed kit production in 2009.
The Moragon Stela is a Spanish two-seat fixed-wing microlight aircraft designed and built Aeromoragan based at Casarrubios del Monte, Spain. [1] The aircraft was supplied as complete or as a kit for amateur construction. [1] The Stela is a two-seat side-by-side high-wing braced monoplane with a composite structure. [1]
Data from Jane's All the World's Aircraft 2000–01 General characteristics Crew: 1 Capacity: 1 Length: 6.2 m (20 ft 4 in) Wingspan: 9.45 m (31 ft 0 in) Height: 2.34 m (7 ft 8 in) Wing area: 12.5 m 2 (135 sq ft) Airfoil: NACA 2412 Empty weight: 265 kg (584 lb) standard 251 kg (553 lb) for competition Max takeoff weight: 540 kg (1,190 lb) Fuel capacity: 50 L (13 US gal; 11 imp gal) with ...
The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules and US light-sport aircraft rules. It features a cantilever low-wing , a two-seats-in- side-by-side configuration enclosed cockpit under a bubble canopy , fixed or retractable tricycle landing gear and a single engine in tractor configuration .