The Martin XB-51 was an American tri-jet ground attack aircraft. It was designed in 1945 and made its maiden flight in 1949. It was originally designed as a bomber by the United States Army Air Forces under specification V-8237-1 and was designated XA-45. The A ground attack classification was eliminated the next year, and the XB-51 designation was assigned instead. The requirement was for low-level bombing and close support. The XB-51 lost out in evaluation to the English Electric Canberra which entered service as the B-57. Design and development The resulting unorthodox design, first flying on 28 October 1949, was (unusually for a combat aircraft) fitted with three engines, General Electric J47s in this case: one at the extreme tail with an intake at the base of the tailfin, and two underneath the forward fuselage in pods. The innovative, variable incidence wings, swept at 35° and with 6° anhedral, were equipped with leading-edge slats, full-width flaps and spoilers instead of ailerons. The combination of variable incidence adjustment and slotted flaps allowed for a shorter takeoff run. Four 954 lb (4.24 kN) thrust Rocket-Assisted Take Off (RATO) bottles with a 14-second burn duration could be fitted to the rear fuselage to improve takeoff performance. Spectacular launches were a feature of later test flights. The main landing gear consisted of dual sets of wheels in tandem in the fuselage, similar to the B-47 Stratojet, with outrigger wheels at the wingtips (originally proved on a modified B-26 Marauder named Middle River Stump Jumper). The B-51 was a large but aerodynamically clean design which incorporated nearly all major systems internally. The aircraft was fitted with a rotating bomb bay, a Martin trademark; bombs could also be carried externally up to a maximum load of 10,400 lb (4,700 kg), although the specified basic mission only required a 4,000 lb (1,814 kg) bombload. Eight 20 mm (.79 in) cannons mounted in the nose would have been installed in production aircraft. Crew provision was for a pilot under a fighter-type bubble canopy and a SHORAN (short-range navigation and bombing system) operator/navigator in a compartment located lower than and to the rear of the cockpit (only a small observation window was provided). Both crew members were provided with a pressurized, air-conditioned environment, equipped with upward-firing ejection seats. The XB-51 was the first Martin aircraft equipped with ejection seats, these being of their own design. Operational history In 1950, the United States Air Force issued a new requirement based on early Korean war experience for a night intruder/bomber to replace the A-26 Invader. The XB-51 was entered, as well as the Avro Canada CF-100 and the English Electric Canberra; the Canberra and the XB-51 emerged as the favorites. The XB-51 was a highly maneuverable aircraft at low level, and substantially faster than the Canberra (its turn-of-speed was faster than most fighter aircraft of the era). However, its load limiting factor of only 3.67 g (36 m/s2) restricted tight turns, and the XB-51s endurance was substantially poorer than the Canberras; this latter proved to be the deciding factor. Additionally, the tandem main gear plus outriggers of the XB-51 was thought unsuitable for the requirement to fly from emergency forward airfields. The Canberra was selected for procurement and the XB-51 program ended. Martin did not end up the loser, however, for they were selected to build the 250 Canberras ordered under the designation B-57A. Furthermore, the rotating bomb bay was incorporated in the B-57. A proposed B-57 Super-Canberra also included XB-51 features, such as swept wing and tailplane. In the end it was never built, mainly because it was a new design and would have taken too long to be put into production, although it promised much better speed and performance. Flight testing for research purposes continued after program cancellation. The second prototype, 46-686, which first flew in 1950, crashed on 9 May 1952 during low-level aerobatics. The first prototype, 46-685 continued to fly, including appearing in the film Toward the Unknown as the Gilbert XF-120 fighter. The surviving prototype was en route to Eglin AFB to shoot additional footage when it crashed during takeoff following a refueling stop in El Paso, Texas, on 25 March 1956. Specifications (XB-51) Crew: 2 Length: 85 ft 1 in (25.9 m) Wingspan: 53 ft 1 in (16.2 m) Height: 17 ft 4 in (5.3 m) Wing area: 548 ft² (50.9 m²) Empty weight: 29,584 lb (13,419 kg) Loaded weight: 55,923 lb (25,366 kg) Max. takeoff weight: 62,457 lb (28,330 kg) Powerplant: 3 × General Electric J47-GE-13 turbojets Performance Maximum speed: 645 mph (1,040 km/h) Range: 1,075 mi (1,730 km) Ferry range: 1,613 mi (2,596 km) Service ceiling: 40,500 ft (12,300 m) Rate of climb: 6,980 ft/min (35.5 m/s) Wing loading: 102 lb/ft² (498 kg/m²) Thrust/weight: 0.28 Armament Guns: 8 × 20 mm (0.79 in) cannon with 1,280 rounds Rockets: 8 × High Velocity Aerial Rockets (HVAR) Bombs: Up to 10,400 pounds of bombs (or eight 5-inch High Velocity Aerial Rockets carried internally) r/max
Posted on: Mon, 12 Jan 2015 01:00:00 +0000
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