B-26 Marauder
See A-26 Invader for the plane known as the B-26 from 1948 to 1962.The
B-26 Marauder was a twin-engine
medium bomber of the
Second World War, built by the
Glenn L. Martin Company.
Peyton M. Magruder led the design team for this aircraft after Martin won a 1939
United States War Department bid.
5,288 were produced between February
1941 and March
1945; 522 of these were flown by the
Royal Air Force and the
South African Air Force.
The first bomber in the
Pacific theater and
Aleutian Islands in 1942, it was also used in the
European Theater of Operations and in the
North African Campaign. The plane distinguished itself as "the chief bombardment weapon on the
Western Front" according to an Army Air Forces dispatch from 1946, and also because the B-26B maintained the lowest loss record of any combat aircraft during World War II. Its loss record stands in sharp contrast to its unofficial nickname "The Widowmaker" – earned due to its high rate of accidental crash during takeoff for the B-26A variation.
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Exploded view of the B-26A |
In
1939, the
United States Army Air Corps issued a specification for a twin-engined medium bomber, Circular Proposal 39-640. Six months later,
Glenn L. Martin Company presented a design to the Air Corps. This design, Martin Model 179, was accepted for production before a prototype even flew, due to the desperate need for medium bombers following the intensification of the war in Europe.
Once the first aircraft came off the production line in November
1940, Martin conducted tests, the results of which were promising. Soon after, it was turned over to the Army Air Corps to be service tested. It went from paper concept to working plane in less than two years.
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The development of the B-26 in illustrated form |
While the B-26 was a fast plane with better performance than the contemporary
B-25 Mitchell, its relatively small wing area and resulting high wing loading (the highest of any aircraft used at that time) led to tricky high-speed landings (approach at 140 mph (225 km/h) and stall at 130 mph (210 km/h)
indicated airspeed). The R-2800 engines were reliable but the electric pitch change mechanism in the propellers required impeccable maintenance and was prone to failure. Failure of the mechanism placed the propeller blades in flat pitch with instant total loss of power. Due to the rotund fuselage, the B-26 engines were placed far outboard and loss of power on one side resulted in a violent snap roll flipping the aircraft on its back. This led to a high number of accidents during takeoff, thus earning B-26 the nickname "Widowmaker" by its pilots (other colorful nicknames included "Martin Murderer," "The Flying Coffin," "B-Dash-Crash," "The Flying Prostitute," (because it had no visible means of support, referring to the small wings) and "The Baltimore Whore" (because the Martin Company was located there) (Higham 1975).
The toll eventually led to a halt in production. During this time a commission of inquiry (led by then-Senator
Harry Truman) was appointed to look into the problem. When Truman and the other commission members arrived at the
Avon Park Bombing Range, they were greeted by the still-burning wreckage of
two crashed Marauders. Indeed, the regularity of crashes by pilots training at
MacDill Field — up to fifteen in one thirty day period — led to the only mildly exaggerated catchphrase, "One a day in Tampa Bay."
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A flight of B-26 Bombers releasing their payloads. |
The resulting aircraft (designated B-26B) had a 6 ft (1.8 m) increase in
wingspan, and other changes, some of which reduced the aircraft's speed. The safety of the B-26B was an immense improvement: it had the lowest attrition rate of any aircraft used during the war. Nevertheless, it remained a challenging plane to fly and continued to be unpopular with potential crews throughout its life.
Like the B-25, the B-26 had been designed for medium-
altitude bombing, but the war brought medium bombers down to treetop level, and later versions of the B-26 were equipped with a side-mounted battery of forward-firing machine guns for
strafing ground targets. The low-level bombing of
Utah Beach by the Marauders during the
Normandy Invasion contributed to the low casualties among the
American assault force.
The B-26 was phased out of Army Air Force service before the end of the war. Their last mission was flown in May
1945.
According to an article in the April edition of
AOPA Pilot on Kermit Weeks's "Fantasy of Flight", the Marauder had a tendency to "hunt" in yaw. This instability is similar to "
Dutch roll". This would make for a very uncomfortable ride, especially for the tail gunner.
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B-26—The first produced model of the B-26, ordered based upon design alone. Flight testing was done on the first few aircraft for about three months after delivery. The armament on this model consisted of two .30 calibre (7.62 mm) and two .50 calibre (12.7 mm)
machine guns; the last model was armed with nearly three times that number. Due to a relatively small wing, the B-26 was difficult to handle at landing speeds. Approximate then cost: $80,226.80/plane (×201)
*
B-26A—Incorporated changes made on the production line to the B-26, including upgrading the two .30 calibre (7.62 mm)
machine guns in the nose and tail to .50 calibre (12.7 mm). 52 B-26As were sent to the
Britain, which were used as the
Marauder Mk I. Approximate then cost: $102,659.33/plane (×139)
*
B-26B—A model with further improvements on the B-26A. 19 were sent to
Britain, which were used as the
Marauder Mk IA. Production blocks of the 1883 planes built:
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AT-23A or
TB-26B—208 B-26Bs converted into target tugs and gunnery trainers designated
JM-1 by the Navy.
**
B-26B—Single tail gun replaced with twin gun; belly-mounted "tunnel-gun" added. (×81)
**
B-26B-1—Improved B-26B. (×225)
**
B-26B-2—
Pratt & Whitney R-2800-39 radials replaced with Pratt & Whitney R-2800-41 radials. (×96)
**
B-26B-3—Larger
carburetor intakes; upgrade to R-2800-43 radials. (×28)
**
B-26B-4—Improved B-26B-3. (×211)
**
B-26B-10 through B-26B-55—Beginning with block 10, the wingspan was increased from 65 ft to 71 ft (19.8 m to 21.6 m), to improve handling problems during landing caused by a high wing load; flaps were added outboard of the engine nacelles for this purpose also. The vertical stabiliser was heightened from 19 ft 10 in to 21 ft 6 in (6 m to 6.6 m). The armament was increased from six to twelve .50 calibre (12.7 mm)
machine guns; this was done in the forward section so that the B-26 could perform
strafing missions. The tail gun was upgraded from manual to power operated. Armour was added to protect the
pilot and
copilot. (×1242)
**
CB-26B—Only 12 B-26Bs were converted into transport aircraft (all were delivered to the Marine Corps for use in the
Philippines).
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B-26C—B-26C was the designation assigned to those B-26Bs that were built in
Omaha, Nebraska instead of
Baltimore, Maryland. 123 B-26Cs were used by the
RAF as the
Marauder Mk II. Approximate then cost: $138,551.27/plane (×1210)
**
TB-26C —Originally designated
AT-23B. Trainer modification of B-26C. (×>300)
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XB-26D— Modified B-26 used to test hot air de-icing equipment, in which heat exchangers transferred heat from engine exhaust to air circulated to the leading and trailing edges of the wing and empennage surfaces. This system, while promising, was not incorporated into any production aircraft made during
World War II. (×1, converted)
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B-26E—Modified B-26B constructed to test the effectiveness of moving the dorsal gun turret from the aft fuselage to just behind the
cockpit. The offensive and defensive abilities of the B-26E was tested against in combat simulations against normal aircraft. Although test showed that gains were made with the new arrangement, the gain was insignificant. After a cost analysis, it was concluded that the effort needed to convert production lines to the B-26E arrangement was not worth the effort. (×1, converted)
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B-26F—Angle of incidence of wings increased by 3.5º; fixed .50 calibre (12.7 mm)
machine gun in nose removed; tail turret and armour around the turret improved. The first B-26F was produced in February of 1944. One hundred of these were B-26F-1-MAs. Starting with 42-96231, a revised oil cooler was added, along with wing bottom panels redesigned for easier removal. 200 of the 300 planes were B-26F-2s and F-6s, all of which were used by the
RAF as the
Marauder Mk III. The Marauder III carried the RAF serials HD402 through HD601 (ex-USAAF serials 42-96329 through 96528). The F-2 had the Bell M-6 power turret replaced by an M-6A with a flexible canvas cover over the guns. The T-1 bombsight was installed instead of the M-series sight. British bomb fusing and radio equipment were provided. (×300)
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B-26G—B-26F with standardised interior equipment. 150 planes used by the
RAF as the
Marauder Mk III. (×893)
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TB-26G—B-26G converted for crew training. Most, possibly all, were delivered to the
United States Navy as the
JM-2. (×57)
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XB-26H—Test aircraft for
tandem landing gear, to see if it could be used on the
Martin XB-48. (×1, converted)
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JM-1P - A small number of JM-1s were converted into photo-reconnaissance aircraft.
* Australia, France, South Africa, United Kingdom, United States (Army Air Corps, Army Air Force, Marine Corps, Navy)
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A B-26F or -G sitting on a runway |
and Jane's Fighting Aircraft of World War II
|crew=7:
2 pilots, bombardier, navigator/radio operator, 3 gunnerslength main=58 ft 3 in | length alt=17.8 m | span main=71 ft 0 in | span alt=21.65 m | height main=21 ft 6 in | height alt=6.55 m | area main=658 ft² | area alt=61.1 m² | empty weight main=24,000 lb | empty weight alt=11,000 kg | loaded weight main=37,000 lb | loaded weight alt=17,000 kg | max takeoff weight main= | max takeoff weight alt= | * Zero-lift drag coefficient: 0.0314 * Drag area: 20.66 ft² (1.92 m²) * Aspect ratio: 7.66>number of props=2 | engine (prop)=Pratt & Whitney R-2800-43 | type of prop=radial engines | power main=1,900 hp | max speed main=287 mph | max speed alt=250 knots, 460 km/h | max speed more=at 5,000 ft (1,500 m) | cruise speed main=216 mph | cruise speed alt=188 knots, 358 km/h) * Landing speed: 104 mph (90 knots, 167) | combat radius main=999 nm | combat radius alt=1,150 mi, 1,850 km | combat radiums more=with 3,000 lb (1,400 kg) of bombs and 1,153 U.S. gal (4,367 L) of fuel | ferry range main=2,480 nm | ferry range alt=2,850 mi, 4,590 km | ceiling main=21,000 ft | ceiling alt=6,400 ft | clim rate main=1,200 ft/min | climb rate alt=6.1 m/s | loading main=46.4 lb/ft² | loading alt=228 kg/m² | power/mass main=0.10 hp/lb | power/mass alt=170 W/kg | * Lift-to-drag ratio: 12.0>guns=12× .50 in (12.7 mm) Colt-Browning machine guns | bombs=4,000 lb (1,800 kg) * B-26 Purchase Orders from 9-20-1939 to 7-15-1943 (PDF), Retrieved October 15, 2005. * * * * O'Mahony, C. (1994) "Me & My Gal -- The Stormy Combat Romance Between a WWII Bomber Pilot and His Martin B-26." Wings December 1994. * * * B26.com (Online Memorial to Marauder Men) * B-26 Historical Society Bibliography Guide * B-26 Martin Marauder Historical Society * USAF Museum * Warbird Alley * Fantasy of Flight's B26 at Fantasy of Flight * 320thbg.org (320th Bomb Group in WWII)Photo galleries* Personal Collection of Captain Joseph J. Merhar, Jr., c. 1943-1945 Aircraft Photos contains several photos of B-26 variants. * Photo of a B-26 in a French museum from German Wikipedia.{{aircontent|related= * Martin XB-27|similar aircraft= * B-25 Mitchell * Vickers Wellington * Douglas A-26 | * B-23 - B-24 - B-25 - B-26 – XB-27 - XB-28 - B-29>lists= * List of bomber aircraft * List of military aircraft of the United States
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