Movatterモバイル変換


[0]ホーム

URL:


Jump to content
WikipediaThe Free Encyclopedia
Search

Vought XF3U

From Wikipedia, the free encyclopedia
icon
This articleneeds additional citations forverification. Please helpimprove this article byadding citations to reliable sources. Unsourced material may be challenged and removed.
Find sources: "Vought XF3U" – news ·newspapers ·books ·scholar ·JSTOR
(July 2024) (Learn how and when to remove this message)
XF3U / XSBU
General information
TypeFighter
National originUnited States
ManufacturerVought
Number built1
History
First flightMay 9, 1933[1]
Developed intoSBU Corsair

TheVought XF3U was theprototype of a two-seat, all-metalbiplanefighter, built by Vought Aircraft Company of Dallas, Texas for theUnited States Navy.

Development and design

[edit]

The XF3U was designed to meet theBureau of Aeronautics 1932Design Specification No. 111, which called for a high-performance fighter with a fixedundercarriage and powered by aPratt & Whitney R-1535 Twin Wasp Junior air-cooled radial engine. Of the seven proposed aircraft the XF3U and theDouglas XFD were chosen. The XF3U was the first all-metal aircraft produced by Vought. The aircraft was also equipped with an enclosedcockpit. During flight testing in 1933, it outperformed the Douglas entry and was chosen the winner.

The XF3U was also redesignated the XSBU, meaning "scout bomber."[2]

Operational history

[edit]

The Navy was no longer interested in two-seat fighters, and therefore only the one XF3U prototype aircraft was built. The XF3U subsequently evolved into adive bomber, and became the XSBU prototype for theSBU-1 Corsair.[1]

The only one every built has a naval bureau number of 9222.[3][4]

Specifications

[edit]

Data fromAngelucci 1987, p. 434.

General characteristics

  • Crew: 2; pilot, navigator
  • Length: 27 ft 10 in (8.4 m)
  • Wingspan: 33 ft 3 in (10.1 m)
  • Height: 11 ft 11 in (3.6 m)
  • Wing area: 295 sq ft (27.4 m2)
  • Empty weight: 3,435 lb (1,558 kg)
  • Max takeoff weight: 5,297 lb (2,402 kg)
  • Powerplant: 1 ×Pratt & Whitney R-1535-80 Twin Wasp Jr. 14-cylinder air-cooled radial engine, 700 hp (518 kW)

Performance

  • Maximum speed: 208 mph (334 km/h, 181 kn)
  • Range: 570 mi (917 km, 500 nmi)
  • Service ceiling: 25,300 ft (7,700 m)
  • Wing loading: 18 lb/sq ft (88 kg/m2)
  • Power/mass: 0.13 hp/lb (0.22 kW/kg)

Armament
3 × .30 in (7.62 mm)machine guns

References

[edit]

Notes

[edit]
  1. ^abAngelucci 1987, p. 434.
  2. ^"Chance Vought/LTV History"(PDF).Environmental Protection Agency (.gov). p. 13. Retrieved9 July 2024.
  3. ^"Appendix 9 - Bureau (Serial) Numbers of Naval Aircraft"(PDF).United States Navy (.mil). p. 530. Retrieved9 July 2024.
  4. ^"Appendix E".NASA (.gov). p. 485. Retrieved9 July 2024.

Bibliography

[edit]
  • Angelucci,Enzo.The American Fighter from 1917 to the present. New York: Orion Books, 1987.ISBN 0-517-56588-9.

External links

[edit]

Media related toVought XF3U at Wikimedia Commons

Manufacturer
designations
By role
Fighters
Scout / Attack
Experimental
Unbuilt
Other
By name
Corsair
Others
United States Navy fighter designations pre-1962
General Aviation
Brewster
Boeing
Curtiss
Douglas
McDonnell
Grumman
Eberhart
Goodyear
Hall
McDonnell
Berliner-Joyce
North American
Loening
Bell
General Motors
Naval Aircraft Factory
Lockheed
Ryan
Supermarine
Northrop
Vought
Canadian Vickers
Lockheed
Wright
CC&F
Convair
1 Not assigned  • 2 Assigned to a different manufacturer's type  • 3 Unofficial  • 4 Unconfirmed
See also:Aeromarine AS  • Vought VE-7
Retrieved from "https://en.wikipedia.org/w/index.php?title=Vought_XF3U&oldid=1257451205"
Categories:
Hidden categories:

[8]ページ先頭

©2009-2025 Movatter.jp