Vultee XP-54 Swoose Goose
Vultee had submitted a proposal in response to a U.S. Army Air Corps request for an unusual configuration. The Vultee design won the competition, beating the Curtiss XP-55 Ascender and the Northrop XP-56 Black Bullet. Vultee designated it Model 84, a descendant of their earlier Model 78. After completing preliminary engineering and wind tunnel tests, a contract for a prototype was awarded on 8 January 1941. A second prototype was ordered on 17 March 1942. Although it appeared to be a radical design, its actual performance was lackluster and the project was subsequently canceled.The XP-54 was designed with a pusher engine in the aft part of the fuselage. The tail was mounted rearward between two mid-wing booms, with the 12-ft propeller between them. The design included a "ducted wing section" developed by the NACA that enabled installation of cooling radiators and intercoolers in the inverted gull wing.
Specifications
General Characteristics
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- Wingspan 39.5ft (12.0m)
- Length 36.1ft (11.0m)
- Height 9.6ft (2.9m)
- Empty Weight 4,297lbs (1,949kg)
- Loaded Weight 8,651lbs (3,924kg)
Performance
- Horse Power/Weight Ratio 0.115
- Wing Loading 28.8lbs/ft2 (140.7kg/m2)
- Wing Area 300.2ft2 (27.9m2)
- Drag Points 2173
Parts
- Number of Parts 53
- Control Surfaces 6
- Performance Cost 287