Navy Hawk |
1934 The Curtiss F11C Goshawk was a 1930s naval biplane that saw limited success but was part of a long line of Curtiss Hawk airplanes built by the Curtiss Aeroplane and Motor Company for the American military. In April 1932 when Curtiss was planning the Model 35B, the US Navy contracted with the manufacturer for an improved derivative of the Model 34C, F6C as the F11C. It contained major changes that included the 600 hp (447-kVV) Wright R-1510-98 engine, single leg cantilever main landing-gear units, a slight increase in the interplane gap, metal rather than fabric-covered control surfaces, and armament based on two 0.3-in (7.62- mm) fixed forward-firing machine guns supplemented by a hardpoint under the fuselage for the carriage of a 474-lb (215-kg) bomb, or an auxiliary fuel tank. Curtiss designed the type as the Model 64 Goshawk, with the US Navy designation XF11C-1 (later XBFC-1 after the adoption of the BF for Bomber-Fighter category). The aircraft was of fabric-covered metal construction, used the wing cell structure of the dismantled YP-23, and was delivered in September 1932. Shortly before ordering the XF11C-1, the Navy had bought a company-owned Model 64A demonstrator. This had a Wright R-1820-78 Cyclone engine, slightly longer main landing-gear legs carrying wheels with low-pressure tires, a tailwheel in place of the tailskid, fabric-covered control surfaces on the tail, and external provision for underwing racks for light bombs as well as an under-fuselage hardpoint for either a 50 US gal (189 L) fuel tank or the crutch that would swing a bomb clear of the propeller disc before release in a dive-bombing attack." Flight trials of this XF11C-2 (later redesignated as the XBFC-2) revealed the need for a small number of minor changes. After making the changes, the XF11C-2 came to be regarded as the prototype for the F11C-2, of which 28 examples were ordered as dual-role fighter-bombers in October 1932. From March 1934 the aircraft were revised with a semi-enclosed cockpit and a number of other modifications before they received the revised designation BFC-2 in recognition of their fighter-bomber or, as the Navy would have it, bomber-fighter role Crew: 1 Length: 22 ft 7 in (6.88 m) Wingspan: 31 ft 6 in (9.6 m) Weight: 9 ft 8.625 in (2.96 m) Wing area: 262 ft2 (24.34 m2) Empty weight: 3,037 lbs (1,378 kg) Max takeoff weight: 4,132 lbs (1,874 kg) Powerplant: 1× Wright R-1820-78 Cyclone radial, 700 hp (522 kW) Maximum speed: 202 mph (325 km/h) Cruise speed: 150 mph (241 kp/h) Service ceiling: 25,100 ft (7,650 m) Rate of climb: 2,300 ft/min (701 m/min) Armament Two .30 cal (7.62 mm) Browning fixed forward-firing machine guns in the forward fuselage, up to 500 lbs (227 kg) disposable stores on three hardpoints USN 83 René Hieronymus Scale 1:72 Building time: 19 hrs. |