Martin XB-51
| Martin XB-51 | ||
|---|---|---|
| Description | ||
| Role | ground attack | |
| Crew | two; pilot and navigator in tandem | |
| First flight | April 17, 1950 | |
| Manufacturer | Martin | |
| Dimensions | ||
| 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 |
| Weights | ||
| Empty | 29,584 lb | 13,419 kg |
| Loaded | 55,923 lb | 25,366 kg |
| Maximum takeoff | 62,457 lb | 28,330 kg |
| Powerplant | ||
| Engines | 3 × General Electric J47-GE-13 turbojets | |
| Thrust | 5200 lbf | 23 kN |
| Performance | ||
| Maximum speed | 645 mph | 1038 km/h |
| Combat range | 1075 miles | 1,730 km |
| Ferry range | 1613 miles | 2,596 km |
| Service ceiling | 40,500 ft | 12,300 m |
| Rate of climb | 6980 ft/min | 2,130 m/min |
| Avionics | ||
| Avionics | ||
| Armament | ||
| Guns | 8 × 20 mm cannon with 1280 rounds | |
| Bombs | 4 × 1600 lb (730 kg) bomb internally, or 2 × 2000 lb (900 kg) bombs externally. Maximum bombload 10,400 lb (4,700 kg). | |
| Rockets | 8 × High Velocity Aerial Rockets (HVAR) | |
The Martin XB-51 was a ground attack aircraft designed to a 1945 United States Army Air Force requirement, and originally 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 resulting design, first flying on October 28, 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. The wings, swept at 35° and with 6° anhedral, were equipped with variable incidence, leading-edge slots, full-width flaps and spoilers instead of ailerons. The main landing gear was dual sets of wheels in tandem in the fuselage, similar to the B-47 Stratojet, with outrigger wheels at the wingtips. 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 (1,800 kg) bombload.
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 XB-51 emerged as the favorites. The XB-51 was a highly maneuverable aircraft at low level, and substantially faster than the Canberra. However, its load limiting factor of only 3.67 G (36 m/s²) restricted tight turns, and the XB-51's endurance was substantially poorer than the Canberra's; 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.
Flight testing for research purposes continued after program cancellation. The second prototype crashed on May 9, 1952 during low-level aerobatics. The other aircraft continued to fly, including appearing in the film Towards the Unknown, until it crashed on takeoff on March 25, 1956. Reference to this Aircraft is mentioned in the 2002 Motion Picture "Hart's War"
External link
| Related content | |
|---|---|
| Related development | |
| Similar aircraft | English Electric Canberra |
| Designation series | |
| Related lists | List of military aircraft of the United States - |
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Categories: U.S. bomber aircraft 1950-1959