The B-26 "Marauder" medium bomber, the winner of a medium bomber design competition, was commissioned before the prototype, so the first production aircraft was also a prototype. Production was constantly slowed down because the necessary design changes had to be introduced literally "in the process." In addition, the aircraft was difficult to master for both technical and flying personnel — its mastery was accompanied by constant accidents. As a result, the plane earned unflattering nicknames such as "Man Killer," "Widow Factory," and "Baltimore Whore." General H.H. Arnold, commander of the U.S. Army Air Forces, wrote of the B-26: "... a very complex, even overly complex, airplane with an enormous amount of electrical equipment." There were even suggestions that the plane be taken out of production. The first production B-26Bs were built in 1940. In 1943 production of the B-26B-55, the last production version of the B-26B, began and ended in February 1944.
The B-26B-55 was an all-metal, twin-engine monoplane with retractable tricycle landing gear. The bombsight was located in the nose cone (some of the aircraft of this modification were equipped with the excellent Norden M-7 bomb sight). The pilots sat side by side in armored seats behind the front armored bulkhead. Four fixed machine guns, 200 rounds each for the lower pair and 250 rounds each for the upper pair, were mounted in two projections on each side of the fuselage behind the pilots. The pilots operated these machine guns. Behind the pilots' seats was a compartment for the navigator and radio operator and a bomb bay. Behind the bomb bay was a dorsal twin machine gun turret with electric drive and 400 rounds of ammunition per gun. A pair of manually operated pintle-mounted machine guns with 250 rounds of ammunition each, located in the tail section, were operated by the plane’s fuselage gunner. The tail gunner's armored mechanized (hydraulically operated) installation also had two machine guns with 800 rounds of ammunition per gun.
A total of 200 B-26B-55s were built.
In Europe, the B-26B was introduced in November 1942. The first results of the raids against the targets in France were so disappointing that the question of taking the Marauders out of production was even raised again. The bombers, flying without fighter cover and from low altitudes, suffered heavy losses. Nevertheless, they played a crucial role in the preparations for the Normandy landings: by May 1944, there were now 10 bombardment groups of B-26s in England, concentrating their efforts in the area of the future amphibious landings. Bridges, railroads, airfields, and coastal batteries were targeted. After the Normandy landings, as the Allied armies advanced across France, the Marauders moved to airfields on the European continent.
1. "American Warplanes of World War II" by David Donald, 1995.
2. С. Kolov "B-26 "Marauder" on military service" Journal "Wings of the Motherland".№1 2001 г
3. Materials of the site airwar.ru
Indicated stall speed in flight configuration: 73...88 mph (118...142 km/h)
Indicated stall speed in takeoff/landing configuration: 67...77 mph (107...124 km/h)
Dive speed limit: 255 mph (410 km/h)
Maximum load factor: 5.0 G
Stall angle of attack in flight configuration: 13 °
Stall angle of attack in landing configuration: 12.5 °
Maximum true air speed at sea level, engine mode - take-off: 365 km/h (227 mph)
Maximum true air speed at 2000 m (6562 feet), engine mode - take-off: 394 km/h (245 mph)
Maximum true air speed at sea level, engine mode - economical maximum: 288 km/h (179 mph)
Maximum true air speed at 5000 m (16404 feet), engine mode - economical maximum: 348 km/h (216 mph)
Service ceiling: 8000 m (26247 feet)
Climb rate at sea level: 6,7 m/s (1319 fpm)
Climb rate at 3000 m: 6,2 m/s (1220 fpm)
Climb rate at 6000 m: 2,9 m/s (571 fpm)
Maximum performance turn at sea level: 22.0 s, at 175 mph (282 km/h) IAS.
Maximum performance turn at 3000 m (9843 feet): 31.0 s, at 165 mph (262 km/h) IAS.
Flight endurance at 3000 m (9843 feet): 3.5, at 300 km/h (187 mph) IAS.
Takeoff speed: 75...85 mph (121..137 km/h)
Glideslope speed: 95..105 mph (153..169 km/h)
Landing speed: 70..80 mph (112..128 km/h)
Landing angle: 11.5 °
Note 1: the data provided is for international standard atmosphere (ISA).
Note 2: flight performance ranges are given for possible aircraft mass ranges.
Note 3: maximum speeds, climb rates and turn times are given for standard aircraft mass.
Note 4: climb rates are given for maximum continuous power, turn times are given for Take-off power.
Engine:
Model: R-1830-92
Maximum power in take-off mode at sea level: 1170 HP
Maximum power in maximum continuous mode at sea level: 1030 HP
Maximum power in economical maximum mode at sea level: 590 HP
Maximum power in take-off mode at 4800 feet (1463 m): 1200 HP
Maximum power in maximum continuous mode at 7000 feet (2134 m): 1050 HP
Maximum power in economical maximum mode at 15000 feet (4572 m): 700 HP
Engine modes:
Take-off (up to 5 minutes): 2700 RPM, 46.0 inch Hg, "Auto-rich"
Maximum continuous (unlimited time): 2550 RPM, 41 inch Hg, "Auto-lean"
Economical maximum (unlimited time): 2325 RPM, 28.0 inch Hg, "Auto-lean"
Oil rated temperature in engine output: 60..75 °C
Oil maximum temperature in engine output: 100 °C
Cylinder head rated temperature: 150..232 °C
Cylinder head maximum temperature: 260 °C
Empty weight: 8029 kg (17700 lb)
Minimum weight (no ammo, 10% fuel): 8828 kg (19462 lb)
Standard weight: 6503 kg (14337 lb)
Maximum takeoff weight: 13337 kg (29403 lb)
Fuel load: 2188 kg (4824 lb) / 3043 l (804 gal)
Useful load: 5308 kg (11702 lb)
Length: 64.8 feet (19.75 m)
Wingspan: 28,96 m (95 feet)
Wing surface: 91,7 m² (987 feet²)
Combat debut: spring 1942