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Boeing B-54

From Wikipedia, the free encyclopedia
Bomber aircraft project by Boeing
B-54
Mockup of the B-54
General information
TypeStrategic bomber
National originUnited States
ManufacturerBoeing
StatusCanceled
Primary userUnited States Air Force (intended)
Number built0
History
Developed fromB-50 Superfortress

TheBoeing B-54 was an Americanstrategic bomber designed byBoeing for use by theUnited States Air Force. Derived from theYB-50C Superfortress, construction of the prototype was canceled before completion, and the aircraft was never flown.

Design and development

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Begun in 1947, the B-54 was the planned production version of theYB-50C prototype. The standardPratt & Whitney R-4360 engines of the normal B-50 bomber were replaced with R-4360-51 Variable Discharge Turbine (VDT) engines, thefuselage was lengthened by over 10 feet (3.0 m) and the wingspan was extended by 20 feet (6.1 m), which required the installation of outrigger landing gear in the first and fourth engine nacelles. Large fuel tanks under the outboard wing section were required to carry an additional 3,000 US gallons (11,000 L; 2,500 imp gal) of fuel to reach the intended 9,300-mile (15,000 km) range; 14 .50-caliber machine guns comprised the specified defensive armament.[1]

On May 29, 1948, contracts were placed by the Air Force for 14 B-54A bombers and 29 RB-54Areconnaissance aircraft.[2][3][4][1] However, on April 18, 1949, the B-54 project was canceled due to the development of better-performing jet aircraft; construction of the prototype B-54A had started at Seattle but was never completed.[1] The cancellation was lambasted by the Seattle press, which claimed that it was a political decision instead of a military one.[5]

Variants

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B-54A
Intended production version of the YB-50C
RB-54A
Reconnaissance version

Specifications

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Data from[2]

General characteristics

  • Crew: 10
  • Length: 111 ft (34 m)
  • Wingspan: 161 ft 0 in (49.08 m)
  • Height: 32 ft 8 in (9.96 m)
  • Gross weight: 230,000 lb (104,326 kg)
  • Powerplant: 4 ×Pratt & Whitney R-4360-51 VDT - "Variable Discharge Turbine"radial piston, 4,300 hp (3,200 kW) each

Performance

  • Maximum speed: 430 mph (690 km/h, 370 kn)
  • Cruise speed: 305 mph (491 km/h, 265 kn)
  • Range: 9,000 mi (14,000 km, 7,800 nmi)
  • Ferry range: 10,562 mi (16,998 km, 9,178 nmi)
  • Service ceiling: 40,000 ft (12,000 m) service

Armament

  • Guns: 14 × .50-caliber machine guns in turrets
  • Bombs: 36,000 pounds (16,000 kg)

See also

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Related development

Aircraft of comparable role, configuration, and era

Related lists

References

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Notes

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Citations

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  1. ^abcJones 1974, p. 183.
  2. ^abNMUSAF 2009
  3. ^Redding and Yenne 1989, p. 117.
  4. ^Andrade, John (1979).U.S. Military Aircraft Designations and Serials Since 1909. Midland Counties Publications.ISBN 0-904597-22-9.
  5. ^Olson 2003, p. 184.

Bibliography

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