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It needed to have folding wings and be able to be towed behind, or carried on the back of a 2.5te truck. It was also required to be towed by other aircraft, to extend the aircraft's range. [1] At least eight projects were submitted to meet the requirement for a lighter aircraft, with Aero's design, the Ae 50, considered the best of the proposals.
The engines were replaced by Pratt & Whitney Canada PW610Fs in 2004 and Eclipse Aviation won the Collier Trophy in February 2006 for the design. A provisional FAA type certification was received on 27 July 2006 and the first delivery occurred on 31 December 2006. The six-seat aircraft has an all-metal airframe with a T-tail and straight wings.
This is a cross-country airplane with many exclusive features including carbon fiber construction, pressurized cabin, high strutless wing, and seating for six. The EA-500 was introduced as an alternative version of the EA-400 with the piston engine replaced by a Rolls-Royce Model 250 -B17F/2 turboprop yielding 450 horsepower (340 kW), weighing ...
An aircraft engine, often referred to as an aero engine, is the power component of an aircraft propulsion system. Aircraft using power components are referred to as powered flight . [ 1 ] Most aircraft engines are either piston engines or gas turbines , although a few have been rocket powered and in recent years many small UAVs have used ...
ADC (from "Aircraft Disposal Company") [3] bought 35,000 war-surplus engines in 1920. Initially produced engines from Renault 70 hp spares. ADC Cirrus. ADC Airdisco; ADC Cirrus; ADC Nimbus, development of Siddeley Puma; ADC Airsix, air-cooled version of Nimbus. Not put into use; ADC BR2 [1] ADC Viper [1] ADC Airdisco-Renault [1]
Data from Junkers aircraft and engines, 1913-1945, Junkers: an aircraft album General characteristics Length: 7.12 m (23 ft 4 in) Wingspan: 10 m (32 ft 10 in) Height: 2.39 m (7 ft 10 in) Wing area: 13.7 m 2 (147 sq ft) Empty weight: 340 kg (750 lb) Gross weight: 590 kg (1,301 lb) Fuel capacity: 95 L (25 US gal; 21 imp gal) Powerplant: 1 × Armstrong Siddeley Genet II five-cylinder air-cooled ...
Data from Worldwide Equipment Guide – Volume 2: Airspace and Air Defense Systems, United States Army Training and Doctrine Command, p. 3-44 General characteristics Crew: 5 (2 pilots, 3 other flight crew) + 10 mission operators Length: 46.6 m (152 ft 11 in) Wingspan: 50.6 m (166 ft 0 in) Height: 14.8 m (48 ft 7 in) Wing area: 300 m 2 (3,200 sq ft) Airfoil: root: TsAGI P-151 (13%); tip: TsAGI ...
The engine consists of three-staged fans, a seven-axial-stage arrangement, and an afterburner. [11] The aircraft has a maximum speed of Mach 1.5. [47] Its engine produces a maximum of 78.7 kN (17,700 lbf) of thrust with afterburner. [11] The more powerful GE F414 and Eurojet EJ200 engines have been suggested as the new engine for the T-50 ...
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