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Aircraft must have a minimum wing area of 66 square feet (6.1 m 2), and an empty weight of 500 pounds or more. The aircraft must also have fixed landing gear, and a fixed pitch propeller. Racers compete in a 3.19-mile (5.13 km) Oval course. [3] Several aircraft were capable of meeting the specifications for Formula One at its creation.
The Air Race E World Cup (also known as Air Race E) is a planned air racing championship run to Formula One rules and adapted for purely electric aircraft.Entrants will design and build electric aircraft to take part in races, flying in groups of 8 around a 5 km oval course marked by 'pylons' at speeds in excess of 250 mph. [1] The series is backed by Airbus, who signed on as founding partner ...
The Sharp DR 90 Nemesis is a Formula One racing aircraft designed by Jon Sharp and built at the Mojave Airport by the Nemesis Air Racing Team. The aircraft is powered by a modified Continental O-200 piston engine. The Nemesis originated as an attempt by Jon Sharp to build a Shoestring racer, with composite skins over a steel frame. Along the ...
Download as PDF; Printable version ... This list of racing aircraft covers aircraft which have been designed or significantly modified to ... Formula One Air Racing ...
The Cassutt Special is a single-seat sport and racing aircraft designed in the United States in 1951 for Formula One air races. Designed by ex-TWA captain Tom Cassutt, it is a mid-wing cantilever monoplane with fixed tailwheel undercarriage. The fuselage and tail are of fabric-covered steel tube construction, and the wings are built from ...
The Sonerai II was designed to be soloed from the rear seat. The aircraft is built around a fabric-covered steel-tube fuselage and tail, [1] with all-aluminum wings [1] and a fiberglass cowl. The plans cost $50 and $57 in 1974. [9] Great Plains Aircraft Supply Company held the rights to the Sonerai series of aircraft until 2015.
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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