XR-11/XH-11 | |
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Role | Twin-rotor helicopterType of aircraft |
National origin | United States |
Manufacturer | Rotorcraft Corporation |
Designer | Gilbert Magill |
First flight | 1947 |
Status | Cancelled |
Primary user | U.S. Army Air Force |
Number built | 1 |
The Rotorcraft XR-11, known by the company as the X-2 Dragonfly, was an American two-seat lightweight helicopter built in the 1940s for evaluation by the United States Air Force by the Rotorcraft Corporation of Glendale, California.
Design and development
The XR-11 was a powered by a 100 hp (75 kW) Continental A100 piston engine driving two three-bladed contra-rotating rotors. Only one was built and first flown in 1947, it was re-designated the XH-11 in 1948, the project was later cancelled.
Variants
- XR-11
- United States Air Force designation later changed to XH-11, one built.
Operators
Specifications
General characteristics
- Crew: 2
- Length: 15 ft 0 in (4.57 m)
- Height: 7 ft 6 in (2.29 m)
- Empty weight: 899 lb (408 kg)
- Max takeoff weight: 1,349 lb (612 kg)
- Powerplant: 1 × Continental A100 , 100 hp (75 kW)
- Main rotor diameter: 2 × 18 ft 0 in (5.49 m)
See also
Related lists
References
Notes
- ^ Andrade 1979, p. 162
- ^ "American airplanes - Ro - Ry". www.aerofiles.com. 25 February 2009. Retrieved 2010-02-18.
Bibliography
- Andrade, John (1979). U.S.Military Aircraft Designations and Serials since 1909. Midland Counties Publications. ISBN 0-904597-22-9.
United States helicopter designations, Army/Air Force and Tri-Service systems | |||||||||
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Numerical sequence used by USAAC/USAAF/USAF 1941–present; U.S. Army 1948–1956 and 1962–present; U.S. Navy 1962–present | |||||||||
Army/Air Force sequence (1941–1962) |
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Tri-Service sequence (1962–present) |
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Not assigned |