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The XP-10 used a 600 hp (447 kW) Curtiss V-1570-15 Conqueror water-cooled V12 engine. To overcome the drag of a radiator (a quite serious issue before the introduction of ethylene glycol ), Curtiss incorporated it into the upper wing.
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 ...
Following rejection of the XP-46, Curtiss put forward their Model 88 in proposals to the United States Army Air Corps. was for an aircraft using the P-40D fuselage and tail assembly with a low drag NACA laminar flow wing, the (at the time under development) Continental I-1430-3 inverted V-12 engine, and eight wing-mounted 0.5 in (12.7 mm) machine guns. [2]
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Curtiss XP-40 in flight. XP-40 fitted with tracked landing gear. In 1937, the 10th P-36A was fitted with a 1,150 hp (860 kW) V-1710-19. Unlike the Model 75I, the resulting XP-40 (Model 75P) did not have a turbo-supercharger, thus the cockpit was not moved back, and the radiator was moved to the ventral position.
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