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Further requirements included a top speed of 250 knots (460 km/h; 290 mph), a cruising speed of 200 knots (370 km/h; 230 mph) and a range of 1,000 nmi (1,900 km; 1,200 mi) with an 800 kg (1,800 lb) bomb load or 2,072 nmi (3,837 km; 2,384 mi) without external armament.
In February 1943, the Imperial Navy staff asked Nakajima Aircraft Company to design a four-engined bomber, capable of meeting an earlier specification set for a long-range, land-based attack plane. The final specification, issued on 14 September 1943, called for a plane with a maximum speed of 320 knots (590 km/h; 370 mph) able to carry a 4,000 ...
The P1Y was designed by the Yokosuka Naval Air Technical Arsenal to Navy specification 15-Shi, [2], calling for a fast bomber with speed matching the Zero, range matching the G4M, a 907 kg (2,000 lb) bombload, and the ability to dive-bomb as well as carry torpedoes. As the result, the construction suffered from excess complexity, difficulty of ...
Unlike the B-1A, the B-1B cannot reach Mach 2+ speeds; its maximum speed is Mach 1.25 (about 950 mph or 1,530 km/h at altitude), [77] but its low-level speed increased to Mach 0.92 (700 mph, 1,130 km/h). [64] The speed of the current version of the aircraft is limited by the need to avoid damage to its structure and air intakes.
The Nakajima G10N Fugaku (Japanese: 富岳 or 富嶽, "Mount Fuji") was a planned Japanese ultra-long-range heavy bomber designed during World War II.It was conceived as a method for mounting aerial attacks from Japan against industrial targets along the west coast (e.g., San Francisco) and in the Midwest (e.g., Detroit, Milwaukee, Chicago, and Wichita) and the northeast (e.g., New York City ...
The Nakajima G5N Shinzan originated due to the Imperial Japanese Navy's interest in developing a long-range attack bomber capable of carrying heavy loads of bombs or torpedoes a minimum distance of 3,000 nmi (5,600 km; 3,500 mi). To meet this requirement, it became apparent a four-engine lay-out would be necessary.
The C6N's first flight was on 15 May 1943, with the prototype demonstrating a speed of 639 km/h (345 kn; 397 mph). [3] Performance of the Homare engine was disappointing, especially its power at altitude, [ 3 ] and a series of 18 further prototypes and pre-production aircraft were built before the Saiun was finally ordered into production in ...
The B5M was designed in response to a 1935 specification for a new bomber ... a speed of not less than 322 km/h (200 mph ... mph, 206 kn) at 2,200 m (7,200 ft) Range ...