Consolidated Vultee XP-81

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Consolidated Vultee XP-81
Type Escort fighter
Manufacturer Consolidated Vultee Aircraft Corporation
Maiden flight 11 February 1945
Status Cancelled
Primary user United States Air Force
Number built 2
Unit cost US$4.6 million for the program[1]

The Consolidated Vultee XP-81 was a development of the Consolidated Vultee Aircraft Corporation to build a single seat, long range escort fighter that combined use of both a turbojet and a turboprop engines. Although promising, the lack of a suitable engine combined with the end of World War II doomed the project.

Contents

[edit] Design and development

Two prototype aircraft were ordered on 11 February 1944 that were designated XP-81. The engine selection was an attempt to couple the high-speed capability of the jet engine with the endurance offered by the propeller engine. The XP-81 was designed to use the General Electric TG-100 turboprop engine (later designated XT-31) in the nose driving a four-bladed propeller and an Allison J33 turbojet in the rear fuselage. The turboprop would be used for normal flight and cruising and the turbojet added for high-speed flight.

[edit] Testing

The first XP-81 (serial 44-91000) was completed in January 1945 but because of developmental problems the turboprop engine was not ready for installation. A decision was then made to mount a complete V-1650-7 Merlin engine package from a P-51D aircraft in place of the turboprop for initial flight tests. This was done in a week and the Merlin-powered XP-81 was sent to the Muroc airbase where it flew for the first time on 11 February 1945. During ten flight test hours, the XP-81 displayed good handling characteristics except for inadequate directional stability due to the longer forward portion of the fuselage (this was rectified by enlarging the vertical tail.[2]

While 13 YP-81 pre-production aircraft had been ordered, the capture of Guam and Saipan removed the need for long-range, high-speed escort fighters and, then, just before VJ Day the contract was cancelled, after 85% of the engineering was completed. The YP-81 was to be essentially the same as the prototype but with a lighter, more powerful TG-110 turboprop engine, the wing moved aft 10 inches (0.25 m), and armament of either six .50 cal (12.7 mm) machine guns or six 20 mm cannon.

After the XP-81 was returned to Vultee Field, the TG-100 turboprop was installed and flight testing resumed. However, the turboprop engine was not able to produce its designed power; producing only the same output as the Merlin (1,490 hp or 1112 kW) with the resultant performance limited to that of the Merlin-powered configuration.

[edit] Cancellation

With the termination of hostilities, the two prototypes continued to be tested until 1947 when they were both ignominiously consigned to a bombing range as photography targets.[3]

[edit] Specifications (XP-81)

Note: Performance is estimated with 'full powered' TG-100 General characteristics

  • Crew: 1
  • Length: 44 ft 10 in (13.67 m)
  • Wingspan: 50 ft 6 in (15.39 m)
  • Height: 14 ft 0 in (4.27 m)
  • Wing area: 425 ft² (39.5 m²)
  • Empty weight: 12,755 lb (5,786 kg)
  • Loaded weight: 19,500 lb (8,850 kg)
  • Max takeoff weight: 24,650 lb (11,180 kg)
  • Powerplant:

Performance

Projected armament

  • Guns:20 mm (0.787 in) cannon
  • Bombs: 2,000 lb (900 kg)

[edit] References

[edit] Notes

  1. ^ Knaack 1978
  2. ^ Green 1961, p. 34.
  3. ^ Winchester 2005, p. 74.

[edit] Bibliography

  • Ginter, Steve. Consolidated Vultee XP-81 (Air Force Legends Number 214). Simi Valley, California: Ginter Books, 2007. ISBN 0-942612-87-6.
  • Green, William. War Planes of the Second World War, Volume Four: Fighters. London: Macdonald & Co.(Publishers) Ltd.,1961. ISBN 0-356-01448-7.
  • Green, William and Swanborough, Gordon. WW2 Aircraft Fact Files: US Army Air Force Fighters, Part 2. London: Macdonald and Jane's Publishers Ltd., 1978. ISBN 0-354-01072-7.
  • Knaack, Marcelle Size. Encyclopedia of US Air Force Aircraft and Missile Systems: Volume 1 Post-World War II Fighters 1945-1973. Washington, DC: Office of Air Force History, 1978. ISBN 0-912799-59-5.
  • Winchester, Jim. The World's Worst Aircraft: From Pioneering Failures to Multimillion Dollar Disasters. London: Amber Books Ltd., 2005. ISBN 1-904687-34-2.

[edit] External links

[edit] See also

Related development

Comparable aircraft

Related lists