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![]() https://en.wikipedia.org/wiki/Curtiss_SB2C_Helldiver The Curtiss SB2C Helldiver is a carrier-based dive bomber aircraft produced for the United States Navy during World War II. It replaced the Douglas SBD Dauntless in US Navy service. The SB2C was much faster than the SBD it replaced. The SB2C Helldiver also saw service with the U.S.Marine Corps (e.g. VMSB-151 AliBaba) flying out of Enjibe Island, Enewetok Atoll on bombing missions. Crew nicknames for the aircraft included the Big-Tailed Beast or just the derogatory Beast, Two-Cee, and Son-of-a-Bitch 2nd Class (after its designation and partly because of its reputation for having difficult handling characteristics). Neither pilots nor aircraft carrier captains seemed to like it. Delays marred its production—by the time the A-25 Shrike variant for the USAAF was deployed in late 1943, the Army Air Forces no longer had a need for a thoroughbred dive bomber. Poor handling of the aircraft was another factor that hampered its service introductions; both the British Royal Navy and the Royal Australian Air Force cancelled substantial orders. The Truman Committee investigated Helldiver production and turned in a scathing report, which eventually led to the beginning of the end for Curtiss. Problems with the Helldiver were eventually ironed out, and in spite of its early problems, the aircraft was flown through the last two years of the Pacific War with a fine combat record. The Helldiver was developed to replace the Douglas SBD Dauntless. It was a much larger aircraft, able to operate from the latest aircraft carriers and carry a considerable array of armament. It featured an internal bomb bay that reduced drag when carrying heavy ordnance. Saddled with demanding requirements set forth by both the U.S. Marines and United States Army Air Forces, the manufacturer incorporated features of a "multi-role" aircraft into the design. The Model XSB2C-1 prototype initially suffered teething problems connected to its Wright R-2600 Twin Cyclone engine and three-bladed propeller; further concerns included structural weaknesses, poor handling, directional instability, and bad stall characteristics. In 1939, a student took a model of the new Curtiss XSB2C-1 to the MIT wind tunnel. Professor of Aeronautical Engineering Otto C. Koppen was quoted as saying, "if they build more than one of these, they are crazy". He was referring to controllability issues with the small vertical tail. The first prototype made its maiden flight on 18 December 1940. It crashed on 8 February 1941 when its engine failed on approach, but Curtiss was asked to rebuild it. The fuselage was lengthened and a larger tail was fitted, while an autopilot was fitted to help the poor stability. The revised prototype flew again on 20 October 1941, but was destroyed when its wing failed during diving tests on 21 December 1941. Large-scale production had already been ordered on 29 November 1940, but a large number of modifications were specified for the production model. Fin and rudder area were increased, fuel capacity was increased, self-sealing fuel tanks were added, and the fixed armament was doubled to four 0.50 in (12.7 mm) machine guns in the wings, compared with the prototype's two cowling guns. The SB2C-1 was built with larger fuel tanks, improving its range considerably. The program suffered so many delays that the Grumman TBF Avenger entered service before the Helldiver, even though the Avenger had begun its development two years later. Nevertheless, production tempo accelerated with production at Columbus, Ohio and two Canadian factories: Fairchild Aircraft Ltd. (Canada), which produced 300 (under the designations XSBF-l, SBF-l, SBF-3, and SBF-4E), and Canadian Car and Foundry, which built 894 (designated SBW-l, SBW-3, SBW-4, SBW-4E, and SBW-5), these models being respectively equivalent to their Curtiss-built counterparts. A total of 7,140 SB2Cs were produced in World War II. Role Dive bomber National origin United States Manufacturer Curtiss-Wright Fairchild (Canada) (SBF) Canadian Car & Foundry (SBW) Designer Don R. Berlin First flight 18 December 1940 Introduction December 1942 Retired 1959 (Italian Air Force) Primary users United States Navy United States Army Air Forces French Naval Aviation Royal Thai Air Force Produced 1943–1945 Number built 7,140 Developed into Curtiss XSB3C The U.S. Navy would not accept the SB2C until 880 modifications to the design and the changes on the production line had been made, delaying the Curtiss Helldiver's combat debut until 11 November 1943 with squadron VB-17 on Bunker Hill, when they attacked the Japanese-held port of Rabaul on the island of New Britain, north of Papua New Guinea. The first version of the SB2C-1 was kept stateside for training, its various development problems leading to only 200 being built. The first deployment model was the SB2C-1C. The SB2C-1 could deploy slats mechanically linked with landing gear actuators, that extended from the outer third of the wing leading edge to aid lateral control at low speeds. The early prognosis of the "Beast" was unfavourable; it was strongly disliked by aircrews due to its size, weight, and reduced range compared to the SBD it replaced. In the Battle of the Philippine Sea, 45 Helldivers, most of which had been deliberately launched from extreme range, were lost when they ran out of fuel while returning to their carriers. Among its major faults, the Helldiver was underpowered, had a shorter range than the SBD, was equipped with an unreliable electrical system, and was often poorly manufactured. The Curtiss-Electric propeller and the complex hydraulic system had frequent maintenance problems. One of the faults remaining with the aircraft through its operational life was poor longitudinal stability, resulting from a fuselage that was too short due to the necessity of fitting onto aircraft carrier elevators. The Helldiver's aileron response was also poor and handling suffered greatly under 90 kn (100 mph; 170 km/h) airspeed; since the speed of approach to land on a carrier was supposed to be 85 kn (98 mph; 157 km/h), this proved problematic. The 880 changes demanded by the Navy and modification of the aircraft to its combat role resulted in a 42% weight increase, explaining much of the problem. U.S. Army and Marine Corps service Built at Curtiss' St. Louis plant, 900 aircraft were ordered by the USAAF under the designation A-25A Shrike. The first ten aircraft had folding wings, while the remainder of the production order omitted this unnecessary feature. Many other changes distinguished the A-25A, including larger main wheels, a pneumatic tailwheel, ring and bead gunsight, longer exhaust stubs, and other Army-specified radio equipment. By late 1943, when the A-25A was being introduced, the USAAF no longer had a role for the dive bomber, as fighter aircraft such as the Republic P-47 Thunderbolt had shown their ability to carry out tactical air support missions with great success. The USAAF transferred 410 Helldivers to the U.S. Marines. The A-25As were converted to the SB2C-1 standard, but the Marine SB2C-1 variant never saw combat, being used primarily as trainers. The remaining A-25As were similarly employed as trainers and target tugs. Specifications (SB2C-4 Helldiver) General characteristics Crew: 2 Length: 36 ft 8 in (11.18 m) Wingspan: 49 ft 9 in (15.16 m) Height: 13 ft 2 in (4.01 m) Wing area: 422 sq ft (39.2 m2) Airfoil: root: NACA 23017; tip: NACA 23009 Empty weight: 10,547 lb (4,784 kg) Gross weight: 16,616 lb (7,537 kg) Powerplant: 1 × Wright R-2600-20 Twin Cyclone 14-cylinder air-cooled radial piston engine, 1,900 hp (1,400 kW) Propellers: 4-bladed constant-speed propeller Performance Maximum speed: 295 mph (475 km/h, 256 kn) at 16,700 ft (5,100 m) Cruise speed: 158 mph (254 km/h, 137 kn) Combat range: 1,165 mi (1,875 km, 1,012 nmi) with 1,000 lb (450 kg) bomb-load Service ceiling: 29,100 ft (8,900 m) Rate of climb: 1,800 ft/min (9.1 m/s) Armament Guns: **2 × 20 mm (0.787 in) AN/M2 cannon in the wings 2 × 0.30 in (7.6 mm) M1919 Browning machine guns in the rear cockpit 4 X 0.50 in (13 mm) M2 Browning machine guns, two each in gunpods mounted on underwing hardpoints (optional) Rockets: 8 × 5 in (130 mm) high velocity aircraft rockets Bombs: in internal bay: 2,000 lb (910 kg) of bombs or 1 × Mark 13-2 torpedo on underwing hardpoints: 500 lb (230 kg) of bombs each * |
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