Hughes XF-11

XF-11
The Hughes XF-11 during a 1947 test flight
Role Reconnaissance
Manufacturer Hughes Aircraft
Designer Howard Hughes
First flight 7 July 1946
Status Cancelled
Primary user U.S. Army Air Force
Number built 2
Developed from Hughes D-2

The Hughes XF-11 was a prototype military reconnaissance aircraft, designed and flown by Howard Hughes for the United States Army Air Force. Despite promise, the XF-11 suffered a crash that nearly killed Hughes. The program never recovered from this setback.

Contents

Design and development

The aircraft was designed to meet the same requirements as the Republic XF-12. Specifications called for a fast, long ranging photo-reconnaissance aircraft. Said to be a scaled-up version of the earlier Hughes D-2, the final design was similar in general appearance to the World War II Lockheed P-38 Lightning.[1] It was a tricycle-gear, twin-engine, twin-boom all-metal monoplane with a pressurized central crew nacelle, with a much larger span and much higher aspect ratio than the P-38's wing.

The XF-11 used Pratt & Whitney R-4360-31 28-cylinder radial engines. Each engine drove a pair of contra-rotating four-bladed, controllable-pitch propellers, which can increase performance and stability, at the cost of increased mechanical complexity.

The Army originally ordered 100 of them for photo reconnaissance. The order was cancelled following the end of World War II, leaving Hughes with two prototypes.

Operational history

The first prototype, tail number 44-70155, piloted by Hughes, crashed on 7 July 1946 while on its maiden flight.[2] An oil leak caused the right-hand propeller controls to lose their effectiveness and the rear propeller subsequently reversed its pitch, disrupting that engine's thrust, which caused the aircraft to yaw hard to the right.[3] Rather than feathering the propeller, Hughes elected to make an emergency landing on the golf course of the Los Angeles Country Club, but about 300 yards short of the course, the aircraft suddenly lost altitude and clipped three houses. The third house was completely destroyed by the fire resulting from the crash and Hughes was nearly killed.[2] The crash is dramatized in the 2004 film The Aviator.

The second prototype was fitted with conventional propellers and flown on 5 April 1947, after Hughes had recuperated from his injuries. This test flight was uneventful and the aircraft proved to be stable and controllable at high speed. However, it lacked low-speed stability as the ailerons were ineffective at low altitudes, and when the Army Air Forces (AAF) evaluated it against the XF-12, testing revealed the XF-11 was harder to fly and maintain, and projected to be twice as expensive to build.[3] A small production order of 98 for the XF-12 went out but the AAF chose the RB-50 Superfortress, and Northrop F-15 Reporter instead, which had similar long-range photo-reconnaissance capability and were available at a much lower cost. The production order was cancelled. When the United States Air Force was created as a separate service in September 1947, the XF-11 was redesignated the XR-11. The surviving XR-11 prototype arrived at Eglin Air Force Base in December 1948 for operational suitability testing.[4]

Specifications (XF-11)

General characteristics

Performance

See also

Related development
Aircraft of comparable role, configuration and era

Related lists

References

Notes
  1. ^ Winchester 2005, p. 222.
  2. ^ a b "Crash of the XF-11." check-six.com. Retrieved: 16 June 2010.
  3. ^ a b Winchester 2005, p. 223.
  4. ^ , "New Ship At Eglin." Fort Walton, Florida Playground News, 30 December 1948, Volume 3, Number 48, p. 1.
Bibliography
  • Barton, Charles. "Howard Hughes and the 10,000 ft. Split-S." Air Classics, Vol. 18, no. 8, August 1982.
  • Winchester, Jim. "Hughes XF-11." Concept Aircraft: Prototypes, X-Planes and Experimental Aircraft. Kent, UK: Grange Books plc., 2005. ISBN 1-84013-309-2.

External links