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Bell X-5
United States — variable-sweep wing research aircraft


Archive Photos

Bell X-5 (AF 50-1838) c.2001 at the National Museum of the United States Air Force, WPAFB, Dayton, Ohio

Overview


The Bell X-5 was the first aircraft capable of changing the sweep of its wings in flight. It was inspired by the untested wartime P.1101 design of the German Messerschmitt company. However, whereas the German design could only be adjusted on the ground, the Bell engineers devised a system of electric motors to adjust the sweep in flight.

  • Role: Research aircraft
  • Manufacturer: Bell Aircraft Corporation
  • Designed by: Robert J. Woods
  • First flight: 20 June 1951
  • Retired: December 1958
  • Primary users: United States Air Force, National Advisory Committee for Aeronautics (NACA)
  • Number built: 2
  • Developed from: Messerschmitt P.1101

Design and Development


The incomplete Messerschmitt P.1101 fighter prototype recovered by US troops in 1945 from the experimental facility at Oberammergau, Germany, was brought back to the United States. Although damaged in transit, the innovative fighter prototype was delivered to the Bell factory at Buffalo, New York where company engineering staff studied the design closely and led by Chief Designer Robert J. Wood, submitted a proposal for a similar design.

Although superficially similar, the X-5 was much more complex than the P.1101, with three sweep positions: 20°, 40°, and 60°, creating an in-flight "variable-geometry" platform. A jackscrew assembly moved the wing's hinge along a set of short horizontal rails, using disc brakes to lock the wing into its in-flight positions. Moving from full extension to full sweep took less than 30 seconds. The articulation of the hinge and pivots partly compensated for the shifts in center of gravity and center of pressure as the wings moved.

Even so, the X-5 had vicious spin characteristics arising from the aircraft's flawed aerodynamic layout, particularly a poorly positioned tail and vertical stabilizer, which in some wing positions, could lead to an irrecoverable spin. This violent stall-spin instability would eventually cause the destruction of the second aircraft and the death of its Air Force test pilot in 1953.

The unfavorable spin characteristics also led to the cancellation of tentative plans by the US Air Force to modify the X-5's design into a low-cost tactical fighter for NATO and other foreign countries.

Operational History


Two X-5s were built (50-1838 and 50-1839). The first was completed 15 February 1951, and the two aircraft made their first flights on 20 June and 10 December 1951. Almost 200 flights were made at speeds up to Mach 0.9 and altitudes of 40,000 ft (12,200 m). One aircraft was lost on 14 October 1953, when it failed to recover from a spin at 60 degree sweepback. USAF Captain Ray Popson died in the crash at Edwards Air Force Base. The other X-5 remained at Edwards and continued active testing until 1955, and remained in service as a chase plane until 1958.

The X-5 successfully demonstrated the advantage of a swing-wing design for aircraft intended to fly at a wide range of speeds. Despite the X-5's stability problems, the concept was later successfully implemented in such aircraft as the General Dynamics F-111 Aardvark, the Grumman F-14 Tomcat and Rockwell B-1 Lancer.

Survivors


The sole surviving X-5 (AF 50-1838) is now at the National Museum of the United States Air Force at Wright-Patterson Air Force Base near Dayton, Ohio. It was delivered to the Museum in March 1958. It is displayed in the Museum's Research & Development Hanger.

Specifications (Bell X-5)


General Characteristics

  • Crew: 1
  • Length: 33 ft 4 in (10.1 m)
  • Wingspan: Unswept: 33 ft 6 in (10.2 m); 60° sweep: 20 ft 10 in (6.5 m)
  • Height: 12 ft (3.6 m)
  • Wing area: 175 sq. ft. (16.26 m².)
  • Empty weight: 6,336 lb (2,880 kg)
  • Max takeoff weight: 9,980 lb (4,536 kg)
  • Powerplant: 1 × Allison J35-A-17 turbojet, 4,900 lbf (21.8 kN)

Performance

  • Maximum speed: 716 mph (1,150 km/h)
  • Range: 750 mi (1,207 km)
  • Service ceiling: 49,900 ft (15,200 m)
  • Thrust/weight: 0.50:1

References


  1. Photos: John Shupek, Copyright © 2009 Skytamer Images. All Rights Reserved
  2. Text, background photos, 3-view: Wikepedia. "Bell X-5." [Online] Available http://en.wikipedia.org/wiki/Bell_X-5, 3 December 2009


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