Model 44 Excalibur | |
---|---|
Role | 32-passenger airliner |
National origin | United States |
Manufacturer | Lockheed Corporation |
Status | Cancelled |
Number built | None |
Developed into | L-049 Constellation |
The Lockheed Model 44 Excalibur was a proposed American airliner designed by Lockheed. The Model 44 was the first four-engined design from the company, a low-wing monoplane with a retractable tricycle landing gear. Originally fitted with twin fins, the design ended up with three fins. It was to be powered by four 1200 hp Pratt & Whitney Twin Wasp radial engines. Pan American Airways was close to ordering the Excalibur when Lockheed abandoned the project to devote its resources into developing the Model 49 Constellation that had been ordered by Trans World Airlines.
In the late 1930s, American aircraft companies such as Boeing and Douglas started developing airliners capable of carrying more passengers at longer ranges than any previous airliner. Douglas, which had the majority of the airliner market with its DC-3, was having trouble finding customers for its proposed Douglas DC-4E (not to be confused with the later DC-4). Boeing also had trouble, as airlines were not interested in its planned 307, which caused its development to be delayed until 1937, when Pan American World Airways and Transcontinental & Western Air provided funding and five orders each. Thus, the 307 first flew on December 31, 1938 and entered service in July 1940.
Around this time, the Lockheed Aircraft Corporation was studying different airliner projects. The first was the Model 27, which had a canard configuration. The other two were the L-104 and L-105. The L-105 was smaller, with 1200 hp engines, and was more conventional than the L-104. These studies led Lockheed's Burbank facility to settle on a design dubbed Model 44, a four-engined airliner that was announced to the public in April 1939. Soon afterwards, the new airliner was dubbed Excalibur. The Excalibur resembled an enlarged Model 10 Electra. It would be powered by four Wright GR-1820 Cyclone 9 radial engines, rated at 1000 hp (746 kW), or four Pratt & Whitney R-1830 Twin Wasp radials. Its wingspan was 95 ft 9 in (29.18 m), its length was 82 ft 6 in (25.15 m), and its projected maximum speed was in the 250-280 mph range (402–451 km/h). Several variants were proposed, to accommodate different passenger loads.