Top speed 731 km/h Wingspan 5.94 m Cruise speed 650 km/h First flight November 1963 | Range 523 km Length 13 m Engine type Turboshaft | |
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Curtiss wright x 19 vtol
The Curtiss-Wright X-19 was an American experimental VTOL tiltrotor airplane of the early 1960s.
Contents
Design and development
In March 1960 the Curtiss-Wright Corporation developed the X-100, a prototype for a new, vertical takeoff transport aircraft. The X-100 had a single turboshaft engine, which propelled two tilting-rotors, while at the tail swivelling nozzles used the engine's exhaust gases to give additional control for hovering or slow flight.
From the X-100 Curtiss-Wright developed the larger X-200, of which the United States Air Force ordered two prototypes designated the X-19A.
The X-19 had high-mounted tandem wings. Each wing mounted two 13 ft (4.0 m) propellers that could be rotated through 90 degrees allowing the aircraft to take off and land like a helicopter. The propellers were driven by twin Avco Lycoming T55-L-5 turboshaft engines mounted in the fuselage.
Operational history
The first flight of the X-19 took place in November 1963 (other sources give 26 June 1964). It was intended that the X-19 would be developed into a VTOL transport aircraft. However the first X-19 was destroyed in a crash on 25 August 1965, and the program was subsequently cancelled.
The second prototype is currently being stored in the restoration facilities at the National Museum of the United States Air Force in Dayton, Ohio.
Specifications (X-19)
General characteristics
Performance
