RON DUPAS COLLECTION
No. 2312. Convair 109 XB-46 (45-59582) US Air Force
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Convair 109 XB-46

01/31/2017. Remarks by Johan Visschedijk: "The Model 109 was Convair's answer to an USAAF specification issued in April 1944 for a high performance all-jet bomber possessing a 1,000 mls (1,609 km) tactical radius, a 500 mph (805 kmh) maximum speed, and a 40,000 ft (12,192 m) ceiling. The proposal submitted on November 6, outlined a conventional design with a Davis-wing shoulder-mounted on an equally slim fuselage which contained the bomb bay and fuel cells. Four 4,000 lb (1,814 kg) st General Electric TG-180 axial-flow turbojets were paired in two wing pod nacelles. The three crew were housed in a pressurized compartment, the two pilots under a fighter-type canopy, and the bombardier in the forward compartment with a glazed nose section. Normal bomb load was 8,000 lb (3,629 kg) and defensive armament consisted of two 0.50 in (12.7 mm) in guns in a remotely-controlled tail turret.

Three prototypes, serialed 45-59582 to 59584 and designated XB-46, were ordered on February 27, 1945, and four other manufacturers also were awarded prototype contracts, North American for its XB-45, and Boeing, Martin, and Northrop for their XB-47, XB-48, and XB-49 respectively. In August, most of Convair's projects were cancelled, but work continued on the XB-46 at a slower pace although funds for two aircraft were diverted to the ill-fated XA-44/XB-53 project. However, Boeing revised its XB-47 design into a swept-wing six-jet concept and it was obvious, barring a design error, that it would outperform the other designs with ease.

The sole XB-46 (45-59582), devoid of military equipment, was thus already outclassed when it first flew on April 2, 1947, flown by E.D. 'Sam' Shannon, with Bill Martin as co-pilot. Despite almost perfect streamlining, its top speed of 545 mph (877 kmh) was below that of the B-45.

The XB-46 was claimed to be the first US aircraft with a complete pneumatic system for the actuation of the landing gear, bomb bay and crew doors, and brakes. Another unusual feature was that to permit almost full-span Fowler-type flaps, roll control was achieved primarily by 20 ft (6.10 m) long spoilers, the ailerons being just 6 ft (1.83 m) in length. There were few problems during flight testing at Muroc with Phase I (company flight tests) completed by September after 14 flights and 23 hours. The major change was to substitute Allison-built General Electric J35-A-3 axial-flow turbojet engines and the XB-46 was then flown to Wright Field. Phil Prophett later became project test pilot and the USAF assigned Captain Glen Edwards to the XB-46, who was subsequently killed testing the Northrop YB-49 and gave his name to the Muroc base.

Following the completion of trials, the elegant XB-46 was flown to Eglin, Florida, and after various tests, was scrapped in mid-1950. A photographic-reconnaissance role was discussed for the B-46 but never implemented."

Created March 10, 2003