Martin XB-51
(Redirected from XB-51)
| B-51 | |
|---|---|
 | |
| Type | Bomber |
| Manufacturer | Glenn L. Martin Company |
| Maiden flight | 1949-10-28 |
| Status | Cancelled in 1951 |
| Number built | 2 |
| Unit cost | US$12.6 million for the program[1] |
The Martin XB-51 was a ground attack aircraft designed to a 1945 United States Army Air Forces 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".
Specifications (XB-51)
General characteristics<h3>- 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: × , 5,200 lbf (23 kN) each
<h3>Performance<h3>- Maximum speed: 645 mph (1,040 km/h)
- Range:
- Combat: 1,075 mi (1,730 km)
- Ferry: 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)
<h3>Armament<h3>
References
- ^ Knaack, MS (1988). Post-World War II bombers, 1945-1973. Office of Air Force History. ISBN 0-16-002260-6.
External links
Related content
<h3>Comparable aircraft<h3>
<h3>Designation sequence<h3>
- A- sequence: XA-42 - XA-43 - A-44 - XA-45
- B- sequence: XB-48 - YB-49 - B-50 - XB-51 - B-52 - XB-53 - B-54
<h3>Related lists<h3>
Categories
U.S. bomber aircraft 1950-1959 | Concept aircraft