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The Boeing B-50
Superfortress was a post-World War II revision of the wartime United States B-29
Superfortress with larger Pratt & Whitney R-4360
radial engines,
a taller vertical stabilizer, and other improvements.
Design
and development
The B-50 program began life as the XB-44
Superfortress. One B-29A-5-BN (s/n 42-93845) was modified by Pratt &
Whitney in 1944 to accept the larger engines; the resulting
engine testbed first flew in May 1945. If the engine
modification had been included in the B-29 program, the resulting
model was to have been known as the B-29D. However, due to other
structural changes that would also be necessary to address the
increased power, weight and fuel consumption, it was decided to
change its military designation to a new model. Since the B-44
program was only for the engine modification, that designation was
not considered, and in December 1945 the program was named B-50
Superfortress.
Officially, the aircraft's new designation was justified by the
changes incorporated into the revised aircraft, but according to Peter M.
Bowers, a long-time Boeing
employee and aircraft designer, and a well-known authority on
Boeing aircraft, "the redesignation was an outright military ruse
to win appropriations for the procurement of an airplane that by
its designation appeared to be merely a later version of an
existing model that was being canceled wholesale, with many
existing examples being put into dead storage."[1]
Revisions to the B-50 (from its predecessor B-29) would result
in a top speed just short of 400 mph (644 km/h), faster
than many World War II propeller-powered fighters. Changes
included:
- Larger engines
- Redesigned engine nacelles and engine mounts
- Enlarged vertical tail and rudder (to maintain adequate yaw
control during engine-out conditions)
- Reinforced wing structure (required due to increased engine
mass, larger gyroscopic forces from larger propeller, greater fuel
load, and revised landing gear loading)
- Revised routing for engine gases (cooling, intake, exhaust and
intercooler ducts; also oil lines)
- Upgraded fire-control equipment (to control remote
turrets)
- Landing gear strengthening (takeoff weight increased from
133,500 lb/60,555 kg to
173,000 lb/78,471 kg)
- Increased fuel capacity (this was largely addressed by adding
underwing fuel tanks).
- Revisions to flight control systems (the B-29 was already
difficult to fly; with its increased weight the B-50 would have
been much harder to hand-fly).
Redesigned with a larger upper fuselage, the B-50 design would
form the basis for the Boeing 377 series of airliners and C-97/KC-97 military transports,
with 816 of the KC-97 built. The B-29 and B-50s would be phased out
with introduction of the jet powered B-47 Stratojet. [2]
The B-50 was nicknamed "Andy Gump" because the redesigned engine
nacelles reminded aircrew of the chinless newspaper comic character
popular at the time.
Operational
history
B-50D-90-BO
48-086 with R-4360 engine differences
visible
Boeing B-50D of 15th Air Force while on detachment to England in
May 1953
Boeing built 371 of the various B-50 models and variants between
1947 and 1953, the tanker versions serving until 1965.
A reconnaissance variant, the
RB-50B (a B-50B conversion) played an important
role in Cold War espionage.
An aerial
refueling tanker conversion designated KB-50
was used in the Vietnam
War.
In 1949, The Lucky Lady II, commanded by Captain
James Gallagher, became the first airplane to circle the world nonstop. This was achieved
by refueling the plane in flight.
Although constructed in relatively small numbers, the B-50 was
the last member of the B-29 family and was one of the last piston-engined bombers built. The B-50 was
retired from its main role as atomic bomber in 1955. A number were
converted into KB-50 tankers and lasted long enough to be deployed
to Southeast Asia in support of tactical operations.
B-50s were grounded and removed completely from inventory when
wreckage of a KB-50 that broke up in flight in 1965 revealed
corrosion problems in the fleet.
No flying examples exist today, although several can be found in
various air museums.
The USAF Strategic Air Command had B-50
Superfortresses (B-50s and RB-50s) in service from 1948 through
1954.
Variants
- XB-44: One B-29A was handed over to Pratt &
Whitney to be fitted with the new Wasp Major 28-cylinder
engines. Initially designated B-29D, this was eventually changed to
B-50A in December 1945. (x1, converted)
- B-50A--First production version of the B-50.
It had new wings that were stronger and lighter than the units on
the B-29. It also had taller vertical tail than the B-29.
(x60)
- B-50B--Increase in gross weight over the A
model, from 168,480 lb (76,420 kg) to 170,400 lb
(77,290 kg). Also included a new type of lightweight fuel
cell. (x45)
- B-50D--Definitive production version of the
B-50. The 7-piece nose cone window was replaced by a single plastic
cone and a flat bomb-aimer's window. Many included the new
boom-type refueling system. (x222)
- DB-50D--Drone director conversion of a B-50D,
to be used with the GAM-63 RASCAL missile. (x1,
converted)
EB-50B with track-tread undercarriage
- EB-50B--Single conversion of a B-50B to be
fitted with a track-tread undercarriage. (x1, converted)
- KB-50--Air to air refueling tanker
conversions of the bomber. (x134, converted)
- KB-50J--Tanker B-50s with improved
performance, via two extra General Electric J47 turbojets
under the outer wings. (x112, converted)
- KB-50K--Tanker conversions of the TB-50H
trainer aircraft. (x24, converted)
- RB-50B--All but one of the B-50Bs were
converted into the recon role. These were fitted with nine cameras
in four stations, weather instruments, and a bomb bay capsule
holding the extra crew members. (x44, converted)
- RB-50E--Special photographic conversions of
the RB-50B, modified at Wichita. (x14, converted)
- RB-50F--Conversions of the RB-50B, fitted with
SHORAN navigation radar for
special missions. (x14, converted)
- RB-50G--Conversions of the RB-50B, fitted with
electronics countermeasures stations along with the SHORAN radar.
(x15, converted)
Boeing WB-50D of 53rd Weather Squadron at
RAF Burtonwood in May 1957
- TB-50A--Trainer conversion of the B-50A. (x11,
converted)
- TB-50D--Trainer conversion of the B-50D. (x11,
converted)
- TB-50H--Newly built trainer planes. (x24)
- WB-50 --Weather reconnaissance conversion of
the B-50.
- WB-50D--Weather reconnaissance conversions of
outdated B-50Ds, fitted with meteorological equipment. (x36,
converted). Some of these flew highly classified missions for
atmospheric sampling between 1953 and 1955 to detect Soviet
detonation of atomic weapons.[3]
- YB-50C--Version to be fitted with the Variable
Discharge Turbine version of the R-4360 engine. None were
built.
- B-54A--Proposed version of the YB-50C.
- RB-54A--Proposed reconnaissance version of the
YB-50C.
Survivors
Only five B-50 type aircraft survive today, from the 371
produced.
- B-50A AF Serial No. 46-0010. This aircraft, "Lucky Lady
II", is disassembled and stored outside at The Air
Museum Planes Of Fame in Chino, CA.
- WB-50D AF Serial No. 49-0310. This aircraft has been moved
indoors after many years outside at the US Air Force Museum in
Dayton, OH.
- WB-50D AF Serial No. 49-0351. This aircraft is displayed
outdoors at Castle Air Museum in Atwater, CA.
- KB-50J AF Serial No. 49-0372. This aircraft is displayed
outdoors at Pima Air & Space Museum in Tuscon, AZ.
- KB-50J AF Serial No. 49-0389. This aircraft is displayed
outdoors at McDill AFB in Tampa, FL.
Operators
United States
Specifications (B-50D)
General characteristics
- Crew: 8: Pilot, co-pilot, flight
engineer, radio/electronic countermeasures operator, two side
gunners, top gunner and tail gunner
- Length: 99 ft 0 in (30.2 m)
- Wingspan: 141 ft 3 in (43.1 m)
- Height: 32 ft 8 in (10.0 m)
- Wing area: 1736 ft² (161.3 m²)
- Empty weight: 80,610 lb (36,560 kg)
- Loaded weight: 121,850 lb (55,270 kg)
- Max takeoff weight:
173,000 lb (78,470 kg)
- Powerplant: 4× Pratt & Whitney R-4360
radial engines,
3,500 hp (2,600 kW)
each
Performance
- Maximum
speed: 395 mph (343 kn, 636 km/h)
- Cruise
speed: 244 mph (212 kn, 393 km/h)
- Combat
radius: 2,100 NM (2,400 mi, 3,860 km)
- Ferry range: 5,000 NM (5,760 mi,
9,270 km)
- Service ceiling: 36,650
ft (11,170 m)
- Rate of
climb: 2,225 ft/min (11.3 m/s)
- Wing
loading: 70.19 lb/ft² (343 kg/m²)
- Power/mass: 0.115 hp/lb
(193 W/kg)
Armament
- Guns:
- Bombs:
- 20,000 lb (9,100 kg) internally
- 8,000 lb (3,600 kg) on external hardpoints
See also
Related development
Related lists
References
Notes
Bibliography
- Jones, Lloyd S. U.S. Bombers, B-1 1928 to B-1 1980s.
Fallbrook, CA: Aero Publishers, 1962, second edition 1974. ISBN
0-8168-9126-5.
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