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Ultralight materials are solids with a density of less than 10 mg/cm 3, including silica aerogels, carbon nanotube aerogels, aerographite, metallic foams, polymeric foams, and metallic microlattices. The density of air is about 1.275 mg/cm 3 , which means that the air in the pores contributes significantly to the density of these materials in ...
The Aero-Works Aerolite 103 is an American single seat, high-wing, pusher configuration ultralight aircraft, designed by Terry Raber and introduced by Aero-Works, Inc, of Millersburg, Ohio, in 1997. The aircraft's model number indicates that it was designed to comply with the Federal Aviation Administration FAR 103 ultralight rules. [1] [4] [5 ...
Belite Aircraft Superlite Belite Ultra Cub. Belite Aircraft was an American aircraft manufacturer based in Wichita, Kansas and founded by James and Kathy Wiebe in 2009. The company specialized in the design and manufacture of ultralight aircraft in the form of kits for amateur construction and ready-to-fly complete aircraft under the US FAR 103 Ultralight Vehicles rules.
The aircraft has an optional powder coated 4130 steel tube frame fuselage covered in doped fabric. The wing is constructed with aluminium tube spars and is also fabric-covered. The kit includes many pre-fabricated parts, including the wing ribs, seat belts and shoulder harnesses, wheels and tires. The manufacturer estimates the construction ...
When the original Flyer was designed there were no suitable lightweight engines available, so the Flyer first fitted two Chrysler powerplants and later two 11.5 hp (9 kW) Solo 209 engines. With the advent of better engines the Ultrastar moved to a single Cuyuna 430 engine producing 35 hp (26 kW).
The Raceair Skylite is an American ultralight aircraft that was designed by Ed Fisher and made available in the form of plans for amateur construction, by Raceair Designs. [ 1 ] [ 2 ] The Skylite design was started in 1988 and the completed aircraft was first shown at Oshkosh in 1991.
The FP-303 was designed by Fisher Aircraft in the United States in 1982 and was intended to meet the requirements of the US FAR 103 Ultralight Vehicles category, including that category's maximum 254 lb (115 kg) empty weight. The design goal was to provide ultralight pilots with an aircraft that was as portable as possible.
Data from Jane's All the World's Aircraft 2010-11 General characteristics Capacity: 2 Length: 6.50 m (21 ft 4 in) Wingspan: 9.20 m (30 ft 2 in) Height: 2.15 m (7 ft 1 in) Wing area: 12.20 m 2 (131.3 sq ft) Empty weight: 265 kg (584 lb) Gross weight: 450 kg (992 lb) limited by European ultralight category Fuel capacity: 50 L (11.0 Imp gal, 13.2 US gal) Powerplant: 1 × Rotax 912 UL-DCDI air ...