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Prototype bomber aircraft by Boeing
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.
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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]
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
- Guns:
- Bombs:
20,000 lb (9,000 kg)
See also
[
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]
Related development
Related lists
References
[
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]
Notes
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]
- ^
Flying Magazine,
August 1945, p. 51.
Bibliography
[
edit
]
- 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
External links
[
edit
]
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