Martin XB-51
1949
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Martin XB-51

The Martin Model 234 was designed originally to meet a US Army Air Force requirement for a close-support bomber, being allocated the designation XA-45. However, it was developed instead as a medium bomber with turbojet power-plant and two prototypes were ordered under the designation XB-51. A cantilever mid-wing monoplane with swept wings and tail surfaces, it was powered by three 2640kg thrust General Electric J47-GE-7 or -13 turbo-jets, one pylon-mounted low on each side of the forward fuselage and the third within the rear fuselage. Other features included pressurised accommodation for the two-man crew, provisi-sions for JATO (jet-assisted take-off) units, and a braking parachute. The first was flown in 1949, but no production order resulted, despite outstanding reliability and handling.

3-View 
Martin XB-51A three-view drawing (452 x 748)


Specification 
 ENGINE3 x 2360kg General Electric J47-GE-13
 WEIGHTS
    Take-off weight25393 kg55982 lb
    Empty weight13431 kg29610 lb
 DIMENSIONS
    Wingspan16.18 m53 ft 1 in
    Length25.93 m85 ft 1 in
    Height5.28 m17 ft 4 in
    Wing area50.91 m2547.99 sq ft
 PERFORMANCE
    Max. speed1038 km/h645 mph
    Cruise speed857 km/h533 mph
    Ceiling12344 m40500 ft
    Range2576 km1601 miles

Martin XB-51


Bob Davis, oji413(@)aol.com, 09.06.2008
I was crew chief on the xb-51 at Edwards AFB in 1955. The xb-51 crashed in El Paso Texas in 1956 killing all on board/ 2 people
Terence John Hunt, tjh34(@)gmx.de, 17.02.2008
Outstanding reliability and handling?????????
In a direct comparison contest, the English Electric "Canberra" twin engined jet bomber flew rings around the B51, and was awarded the USAF contract. It was built in relatively large numbers by Martin as the B-57.

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