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Very shortly after the end of World War II Convair began the design of a turbojet-powered medium bomber, gaining a contract for three XB-46 prototypes from the US Army Air Force. Of all-metal construction, the XB-46 was of high-wing cantilever monoplane configuration, had a slim oval-section fuselage, conventional tail unit, retractable tricycle landing gear and was designed to accommodate a crew of three. Power-plant consisted of four turbojet engines, these being mounted in pairs.
 | A three-view drawing (650 x 990) |
First flown on 2 April 1947, the XB-46 was handed over to the newly-formed US Air Force in late 1947, attaining an average speed of 858km/h during its delivery flightto Wright Field at Daytona, Ohio. Despite this performance the XB-46 remained a one-off prototype, the USAF ordering the Boeing B-47 Stratojet into production.
| CREW | 3 |
| ENGINE | 4 x turbo-jet General Electric TG-180(J35), 1814kW |
| WEIGHTS |
| Take-off weight | 41278 kg | 91003 lb |
| Empty weight | 21782 kg | 48021 lb |
| DIMENSIONS |
| Wingspan | 34.44 m | 112 ft 12 in |
| Length | 32.24 m | 105 ft 9 in |
| Height | 8.53 m | 27 ft 12 in |
| Wing area | 102.1 m2 | 1098.99 sq ft |
| PERFORMANCE |
| Max. speed | 813 km/h | 505 mph |
| Cruise speed | 700 km/h | 435 mph |
| Ceiling | 13105 m | 43000 ft |
| Range | 4820 km | 2995 miles |
| ARMAMENT | 9000kg of bombs |
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