XP-55 Ascender

The Curtiss-Wright XP-55 Ascender (company designation CW-24) is 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. An unusual design for its time, it had a canard configuration with a rear-mounted engine, and two vertical tails at end of swept wings. Because of its pusher design, it was satirically referred to as the "Ass-ender". Like the XP-54, the Ascender was designed for the 1,800 hp Pratt & Whitney X-1800 24-Cylinder H-engine, but was redesigned after that engine project was canceled. It was also the first Curtiss fighter aircraft to use tricycle landing gear. Development of the Ascender was cancelled when testing revealed it to be inferior to conventional fighter aircraft, and the first jet fighters were operational.
Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.
- Manufacturer
- Curtiss-Wright
- Category
- Fighters
Specifications
- Cruise speed
- 340 kt
- Max speed
- 390 kt
- Range
- 552 nm
- Service ceiling
- 34,600 ft
- Max takeoff weight
- 7,930 lb
- Empty weight
- 6,354 lb
- Powerplant
- Allison V-1710-95
- Engines
- 1
- Seats
- 1
- Length
- 29.6 ft
- Wingspan
- 40.6 ft
- Height
- 10 ft
- Number built
- 3
Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).
Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.