During World War II, the United States put all its effort into strengthening its air forces, prioritizing the strangest ideas and proposals for fighters that manufacturers could conceive and build within a couple of years. One of the most bizarre examples was the Northrop XP-56 Black Bullet, which ultimately was too innovative to be produced.

In the early days of the conflict, the United States Air Corps was well aware that potentially unfriendly countries were already flying too fast and too high. Not to mention their well-armed and smoothly maneuverable aircraft that totally outclassed every model currently built in the US.

The need for advanced pursuit aircraft became palpable as air combat exploded in Europe, and Germany showcased its technological superiority. Even the Japanese aircraft were unpaired at the time.

The initial idea for the XP-56 was quite radical for 1939. It was to have no horizontal tail, only a small vertical tail, used an experimental engine, and be produced using a novel metal, magnesium. The aircraft was to be a wing with a small central fuselage added to house the engine and pilot. It was hoped that this configuration would have less aerodynamic drag than a conventional airplane.

The idea for this single-seat aircraft originated in 1939 as the Northrop N2B model. It was designed around the Pratt & Whitney liquid-cooled X-1800 engine in a pusher configuration driving contra-rotating propellers. The U.S. Army ordered Northrop to begin design work on 22 June 1940, and after reviewing the design ordered a prototype aircraft on 26 September 1940. Shortly after design work had begun, Pratt & Whitney, however, stopped development of the X-1800. The Pratt & Whitney R-2800 engine was substituted, although it was considered not entirely suitable. The new, 2,000-horsepower (1,500 kW) engine was 200 horsepower (150 kW) more powerful, but it had a larger diameter and required a larger fuselage to house it. This change delayed the program by five months. It was expected that the new engine would require a 2,000 lb (910 kg) weight increase and cost 14 mph (23 km/h) in top speed.

Since this tailless design was novel and considered high risk, it was decided to construct a small, lightweight plane of similar configuration for testing called the Model N-1M. In parallel with the design of the XP-56, successful flight trials of the configuration were conducted utilizing this airframe, confirming the basic layout. Two small Lycoming engines powered this aircraft. These trials confirmed the stability of the radical design and, upon review, the Army decided to construct a second prototype, which was ordered on 13 February 1942.

Northrop constructed the XP-56 using magnesium alloy for the airframe and skin, because aluminium was forecast to be in short supply due to wartime demands. At the time there was little experience with magnesium aircraft construction. Because magnesium cannot be easily welded using conventional techniques, Northrop hired Vladimir Pavlecka to develop the heliarc welding technique for magnesium alloy. (Later it was discovered that in the 1920s General Electric had already developed similar techniques.

Sources: YouTube; Wikipedia

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