General info for XP-55

• Country USA
• Vehicle role Fighter
• Rank 2

• Battle rating in
  • arcade battles 3.7
  • realistic battles 3.7
  • simulator battles 3

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Wiki info about XP-55

Official War Thunder wiki

Curtiss-Wright XP-55 Ascender single-engine army interceptor fighter prototype The Curtiss-Wright XP-55 (company designation CW-24) prototype interceptor fighter was developed to meet the requirements of Proposal R-40C, issued by the United States Army Air Corps on November 27, 1939. It called for the creation of a fighter outperforming all existing models in speed, rate of climb, manoeuvrability, armament, and pilot visibility. In addition, it required that the new fighter would have small production and maintenance costs. The R-40C requirements specifically mentioned that the aircraft to be created should have an unconventional aerodynamic configuration. The aircraft created by the Curtiss-Wright designers had a canard configuration with swept wings and a pusher propeller. The swept wings had ailerons and flaps, and small fins with rudders were fitted at the wing tips. The horizontal empennage was under the wings. The CW-24 had a tricycle landing gear with a nosewheel. The Curtiss Company also proposed using the new, yet untested Pratt & Whitney X-1800 liquid-cooled engine, mounted behind the pilot and driving the pusher propeller. On 10 July 1942, the US Army Air Corps ordered three prototype aircraft, which received the army designation of ХР-55. Since there was much difficulty with the further development of the Pratt & Whitney X-1800 engine, the company's specialists decided to use an Allison V-1710-95 twelve-cylinder, V-type, liquid-cooled engine, which produced a takeoff power of 1,275 hp. The aircraft's armament consisted of four 12.7 mm Colt-Browning AN-M2.5 machine guns with 200 rounds each. Two 20 mm Bendix-Hispano AN-M2C cannons, with 200 rounds each, were planned to be mounted on this series, as well. The ХР-55 prototype (Ser No. 42-78845) performed its first flight on July 19, 1943, at Scott Field Air Force Base, not far from the Curtiss-Wright factory in St. Louis. The tests showed that the ХР-55 had satisfactory controllability when flying horizontally or gaining altitude, but the pilots experienced some inconveniences when landing or flying at low speeds, as they could not feel any load on the elevator. There were also some cooling problems with the Allison V-1710-95 engine, which was located in the rear section of the airframe. The ХР-55's characteristics were not particularly outstanding, and even inferior to those of fighters of classic conventional configuration already in service. Besides, it became quite evident by early 1944 that further fighter development would employ not piston but turbojet engines. As a result, no order for full-scale production followed, and all work on the ХР-55 was discontinued.