Vought XF5U

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XF5U
The XF5U-1 during testing
Role Fighter
Manufacturer Vought
Designer Charles H. Zimmerman
First flight 1943
Status Cancelled 17 March 1947
Primary user United States Navy
Number built 2
Developed from Vought V-173

The Vought XF5U "Flying Flapjack" was an experimental

flapjack/pancake, hence its nickname) serving as the lifting surface.[1]
Two piston engines buried in the body drove propellers located on the leading edge, at the wingtips.

Design and development

A developed version of the original

aspect ratio aircraft with low takeoff and landing speeds but high top speed.[2] The aircraft was designed to keep the low stall speed and high angle of attack from the V-173 prototype while providing for better pilot visibility, cockpit comfort, less vibration, and provisions to install armament. This included a cockpit redesign moving the cockpit from the leading edge of the wing to a nose nacelle that extended further in front of the leading edge. The arrestor hook was changed to a dorsal hook that would diminish the drag from the apparatus.[3]

propellers to actively cancel the drag-causing tip vortices.[4]
The propellers are arranged to rotate in the opposite direction to the tip vortices, with the aim of retaining the higher-pressure air below the wing. With this source of drag eliminated, the aircraft would fly with a much smaller wing area, and the small wing would yield high maneuverability with greater structural strength.

The propellers envisioned for the completed fighter — unlike the torque-reducing

Vought F4U-4 Corsair. An ejection seat was fitted to allow the pilot to clear the massive propellers in the event of an in-flight emergency.[2] Although the prototype was unarmed, a combination of six M2 Browning 50-caliber machine guns or four M3 20 mm cannons would be mounted in the wing roots in service.[2]

Testing and evaluation

The XF5U design was promising: specifications given at the time promised great maneuverability and speeds up to 452 mph (727 km/h).

Smithsonian Museum for display. Although two aircraft were constructed, a lone XF5U-1 underwent ground runs but never overcame vibration problems. Taxi trials at Vought's Connecticut factory culminated in short "hops" that were not true flights.[7][8] The only completed XF5U-1 proved to be so structurally solid that it had to be destroyed with a wrecking ball.[9]

Specifications (XF5U-1)

3-view line drawing of the Vought XF5U

General characteristics

  • Crew: 1 pilot
  • Length: 28 ft 7 in (8.73 m)
  • Wingspan: 32 ft 6 in (9.91 m)
  • Height: 14 ft 9 in (4.50 m)
  • Wing area: 475 sq ft (44.2 m2)
  • Empty weight: 13,107 lb (5,958 kg)
  • Gross weight: 16,722 lb (7,600 kg)
  • Max takeoff weight: 18,772 lb (8,533 kg)
  • Powerplant: 2 ×
    Pratt & Whitney XR-2000
    -2 radial engine, 1,350 hp (1,007 kW) each

Performance

  • Maximum speed: 452 mph (727 km/h, 393 kn) at 28,000 ft (8,500 m) (estimated)[6]
  • Stall speed: 20 mph (32 km/h, 17 kn)
  • Range: 710 mi (1,142 km, 620 nmi)
  • Service ceiling: 34,500 ft (10,516 m)
  • Rate of climb: 3,120 ft/min (15.8 m/s) or 910 m/min
  • Wing loading: 39.2 lb/sq ft (191 kg/m2)

Armament

See also

Related development

Aircraft of comparable role, configuration, and era

Related lists

References

Notes

  1. ^ Chant 1984, p. 53.
  2. ^ a b c d Winchester Concept Aircraft 2005, p. 247.
  3. ^ Naval Fighters Number Twenty One Chance Vought V-173 and Xf5U-1 Flying Pancakes. Steve Ginter. 1992. pp. 15, 23.
  4. ^ Norton 2008, p.165
  5. ^ Naval Fighters Number Twenty One Chance Vought V-173 and Xf5U-1 Flying Pancakes. Steve Ginter. 1992. p. 15.
  6. ^ a b "Airplane characteristics and performance" (PDF). Retrieved 2023-12-17.
  7. ^ Winchester X-Planes 2005, p. 222. Suggestions of first XF5U flight were confused the V-173 test flying that continued into 1945.
  8. ^ Jerram 1980, p. 71.
  9. ^ Jerram 1980, p. 72.
  10. ^ "It became known why the USA created the world's slowest XF5U plane — SUNDRIES". 8 September 2022.

Bibliography

External links