|X-19 in hovering flight|
|Role||Experimental VTOL Transporter|
|First flight||November 1963|
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.
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.
- Crew: 2
- Payload: 1,200 lb (544 kg)
- Length: 42.08 ft (12.83 m)
- Wingspan: 19.5 ft (forward) / 21.5 ft (aft) (5.94 m / 6.55 m)
- Height: 17.17 ft (5.2 m)
- Empty weight: 9,775 lb (4,425 kg)
- Max. takeoff weight: 13,660 lb (6,196 kg)
- Powerplant: 2 × Avco Lycoming T55-L-5 turboshaft, 2,200 shp (1,640 kW) each
- Aircraft of comparable role, configuration and era
- Apostolo 1984, p. 63.
- "Aircraft list." National Museum of the United States Air Force. Retrieved: 17 June 2012.
- Apostolo, Giorgio. The Illustrated Encyclopedia of Helicopters. New York: Bonanza Books, 1984. ISBN 0-517-439352.
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