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N 1] The Hall Aluminum Aircraft Company submitted the only seaplane design; [3] a single prototype was ordered by the Navy for evaluation on June 30, 1934. Given the designation XPTBH-1, [5] it became the only aircraft to receive three mission-type letters under the U.S. Navy's designation system used between 1922 and 1962. [6] [7] [8]
Data from Ultralight News, Pilot Mix. General characteristics Crew: one Capacity: one (ultralight configuration) Length: 17 ft 3 in (5.26 m) Wingspan: 27 ft 5 in (8.36 m) Height: 5 ft 0 in (1.52 m) varies by main landing gear wheel diameter Wing area: 123 sq ft (11.4 m 2) Empty weight: 254 lb (115 kg) Gross weight: 540 lb (245 kg) Fuel capacity: 5 US gallons (19 litres) Powerplant: 1 × Rotax ...
It is made from 7075-T6 aluminum tubing, with the control bar and kingpost made from 6061-T6 aluminum. The single-surface wing is covered in Dacron sailcloth. Its 39.0 ft (11.9 m) span wing is cable braced from a single kingpost. The nose angle is 115°, wing area is 330 sq ft (30.7 m 2) and the aspect ratio is 5:1. Pilot hook-in weight range ...
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 Aero Designs Pulsar is an American two-seat, low wing, ultralight and homebuilt aircraft that was designed by Mark Brown and first produced by Aero Designs of San Antonio, Texas, introduced in 1985. When it was available the Pulsar was supplied as a ready-to-fly aircraft and as a kitplane for amateur construction. [1] [2]
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The F1 Rocket is a tandem two-seat low-wing cantilever monoplane built mainly in aluminum. [1] The Rocket has a titanium fixed conventional landing gear with a tailwheel. . Designed to be built with a range of nose-mounted engines between 235 and 350 hp (175 and 224 kW) the prototype has a Lycoming IO-540 with a three-bladed propelle
The aircraft has been designed to standard light aircraft FAR-23 static load requirements with the wings supporting more than 10,000 pounds in sandbags during the tests. [7] Intended for the US experimental home-built and light-sport aircraft categories, in 2012 the company estimated the total price to purchase and build the aircraft to be ...