Curtiss-Wright XP-55 Ascender
One of the unique concepts made by the Curtiss-Wright Corporation, the XP-55 had a unique pusher prop design
Controls ar as any conventional plane, with the addition of VTOL down for landing
Tips for landing: Go at an angle between 0* degrees and -10* degrees
______________________________________Wikipedia________
The Curtiss-Wright XP-55 Ascender (company designation CW-24) was a 1940s United States prototype fighter aircraft built by Curtiss-Wright. Along with the Vultee XP-54 and Northrop XP-56, it resulted from United States Army Air Corps proposal R-40C issued on 27 November 1939 for aircraft with improved performance, armament and pilot visibility over existing fighters; it specifically allowed for unconventional aircraft designs. A highly unusual design for its time, it had a canard configuration, a rear mounted engine, swept wings and two vertical tails. Because of its pusher design, it was sarcastically referred to as the "Ass-ender". Like the XP-54, the Ascender was initially designed for the Pratt & Whitney X-1800 engine and had to be redesigned when that engine project was cancelled. It was also the first Curtiss fighter aircraft to use tricycle landing gear
Specifications
General Characteristics
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- Wingspan 42.4ft (12.9m)
- Length 40.6ft (12.4m)
- Height 11.4ft (3.5m)
- Empty Weight 6,840lbs (3,103kg)
- Loaded Weight 17,001lbs (7,711kg)
Performance
- Horse Power/Weight Ratio 0.117
- Wing Loading 46.2lbs/ft2 (225.6kg/m2)
- Wing Area 368.0ft2 (34.2m2)
- Drag Points 3376
Parts
- Number of Parts 118
- Control Surfaces 12
- Performance Cost 489
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