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https://en.wikipedia.org/wiki/Curtiss_A-12_Shrike
The Curtiss A-12 Shrike was the United States Army Air Corps' second monoplane ground-attack aircraft, and its main attack aircraft through most of the 1930s. It was based on the A-8, but had a radial engine instead of the A-8's inline, water-cooled engine, as well as other changes. The Model 60 was developed from advancements of the A-8 and the experimental YA-10. However, it became obsolete after a short use period, mainly because of fast-improving aviation technology, as well as the USAAC's desire for multi-engined attack aircraft. The most obvious difference between the A-12 and the A-8 is the air-cooled, radial engine in the A-12, which replaced the A-8's inline, water-cooled engine. This was a response to the USAAC's move toward a preference for radial engines, especially in attack aircraft. The rationale behind this preference is that the radial engine has a lower profile, making it less vulnerable to ground fire, and a simpler cooling mechanism, which is also less prone to groundfire, as well as overall maintenance problems. These aircraft retained the open cockpit introduced in the A-8 production batch, and carried the same weapons load. In an attempt to improve pilot/observer co-operation, the rear cockpit was moved forward sufficiently for its glazed covering to form a continuation of the fuselage decking behind the pilot's cockpit. Nine USAAF A-12s were still in service at Hickam Field on 7 December 1941, but they saw no combat. Role Ground-attack aircraft Manufacturer Curtiss Introduction 1933 Retired 1942 Primary users United States Army Air Corps Nationalist Chinese Air Force Number built 46[1] Developed from XA-8 Shrike YA-10 Shrike Specifications (A-12 Shrike) General characteristics Crew: 2 Length: 32 ft 3 in (9.83 m) Wingspan: 44 ft 0 in (13.41 m) Height: 9 ft 4 in (2.84 m) Wing area: 284 ft² (26.38 m²) Empty weight: 3,898 lb (1,768 kg) Max. takeoff weight: 5,756 lb (2,611 kg) Powerplant: 1 × Wright R-1820 "Cyclone" 9-cylinder air-cooled radial engine, 690 hp (515 kW) Performance Maximum speed: 177 mph (154 knots, 285 km/h) Range: 521 mi (453 nmi, 838 km) Service ceiling: 15,150 ft (4,620 m) Armament Guns: 4 × forward-firing .30 in (7.62 mm) machine guns 1 × aft-firing .30 in (7.62 mm) machine gun Bombs: 4 × 122 lb (55 kg) bombs on underwing racks or 10 × 30 lb (13.6 kg) fragmentation bombs in chutes on either side of the main fuel tank * |
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