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Boeing XB-39 Superfortress - Wikipedia

Boeing XB-39 Superfortress

The Boeing XB-39 Superfortress was a United States prototype bomber aircraft, a single example of the B-29 Superfortress converted to fly with alternative powerplants. It was intended to demonstrate that the B-29 could still be put into service even if the first choice of engine , the air-cooled Wright R-3350 radial engine , ran into development or production difficulties.

XB-39 Superfortress
Boeing XB-39 serial number: 41-36954
Role Heavy bomber
Manufacturer Boeing
First flight 9 December 1944
Primary?user United States Army Air Forces
Produced 1944
Number built 1
Developed from Boeing B-29 Superfortress

Design and development

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Starting life as the first YB-29 delivered to the United States Army Air Forces , it was sent in November 1943 to the Fisher Body Aircraft Development Section of General Motors to be converted to use Allison V-3420 -17 liquid-cooled W24 (twin- V12 , common crankcase) inline engines. [1] Fisher was chosen for the modification as it was familiar with the engine, as it was to power the P-75 Eagle that they were then developing. Testing on it began in early 1944.

Further development of the engine and the aircraft was delayed by a series of changes in the planned turbosuperchargers , as the originally specified GE Type CM-2 two-stage turbosupercharger became unavailable due to demands on GE's production of its other turbosuperchargers. Other turbosuperchargers were considered, but the result was that the first flights of the XB-39 had to be made without any turbosuperchargers at all.

Operational history

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General Motors modified B-29 to use Allison V-3420 engines

Fisher finally focused again on the B-39. The first flight of the B-39 was made on 9 December 1944 at Cleveland, Ohio. The initial flight tests of the B-39, without turbosuperchargers installed, were impressive. However, the B-39 program was by now seriously delayed, and the flawed R-3350 B-29s had already been rushed into combat in June 1944.

Despite continuing problems with the B-29s, the aircraft was functioning well enough in combat that it no longer made any sense to shift resources in the manufacturing base to a new engine for the B-29 and so the B-39 was not ordered into production.

Specifications (XB-39)

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General characteristics

  • Crew: 10: pilot , co-pilot, flight engineer , bombardier , navigator , radio operator, side gunners (two), top gunner, and tail gunner
  • Length: 99?ft 0?in (30.18?m)
  • Wingspan: 141?ft 3?in (43.05?m)
  • Height: 27?ft 9?in (8.46?m)
  • Wing area: 1,736?sq?ft (161.3?m 2 )
  • Empty weight: 74,500?lb (33,800?kg)
  • Gross weight: 120,000?lb (54,000?kg)
  • Max takeoff weight: 133,500?lb (60,560?kg)
  • Powerplant: 4 × Allison V-3420 -11 liquid-cooled W24 (double-vee) engines, 2,100 hp (1,600 kW) each

Performance

  • Maximum speed: 405?mph (648?km/h, 351?kn)
  • Range: 6,290?mi (10,060?km, 5,460?nmi)
  • Service ceiling: 35,000?ft (11,000?m)
  • Wing loading: 69.12?lb/sq?ft (337.5?kg/m 2 )
  • Power/mass : 0.073 hp/lb (121 W/kg)

Armament

See also

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Related development

Related lists

References

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Notes

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  1. ^ Flying Magazine, August 1945, p. 51.

Bibliography

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  • Jones, Lloyd S. U.S. Bombers, B-1 1928 to B-1 1980s . Fallbrook, California: Aero Publishers, 1962, second edition 1974. ISBN  0-8168-9126-5 .
  • Whitney, Daniel. Vee's For Victory! . Atglen, Pennsylvania: Schiffer Military History, 1998. ISBN  0-7643-0561-1
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