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Lockheed Constellation

Constellation
C-69.jpg
A USAF C-69, the military version of the Constellation
Role Airliner and transport
Manufacturer Lockheed
First flight January 9, 1943
Introduction 1943 with USAAF
1945 with TWA
Retired 1990s, airline service
1978, military
Status In very limited service
Primary users Trans World Airlines
Eastern Air Lines
Pan American World Airways
Air France
Produced 1943–1958
Number built 856
Developed from L-044 Excalibur
Variants L-049 Constellation
C-69 Constellation
L-649 Constellation
L-749 Constellation
L-1049 Super Constellation
C-121/R7V Constellation
R7V-2/YC-121F Constellation
EC-121 Warning Star
L-1649A Starliner
Developed into Lockheed XB-30 (Unbuilt)

The Lockheed Constellation ("Connie") was a propeller-driven, four-engined airliner built by Lockheed Corporation between 1943 and 1958 at Burbank, California. Lockheed built 856 in numerous models—all with the same triple-tail design and dolphin-shaped fuselage. Most were powered by four 18-cylinder Wright R-3350 Duplex-Cyclones. The Constellation was used as a civil airliner and as a military and civilian air transport, seeing service in the Berlin and the Biafran airlifts. Three of them served as the presidential aircraft for Dwight D. Eisenhower.

Lockheed had been working on the L-044 Excalibur, a four-engine, pressurized airliner, since 1937. In 1939, Trans World Airlines, at the instigation of major stockholder Howard Hughes, requested a 40-passenger transcontinental airliner with a range of 3,500 mi (5,630 km)—well beyond the capabilities of the Excalibur design. TWA's requirements led to the L-049 Constellation, designed by Lockheed engineers including Kelly Johnson and Hall Hibbard.Willis Hawkins, another Lockheed engineer, maintains that the Excalibur program was purely a cover for the Constellation.

The Constellation's wing design was close to that of the P-38 Lightning, differing mostly in size. The triple tail kept the aircraft's height low enough to fit in existing hangars, while features included hydraulically boosted controls and a de-icing system used on wing and tail leading edges. The aircraft had a maximum speed of over 375 mph (600 km/h), faster than that of a Japanese Zero fighter, a cruise speed of 340 mph (550 km/h), and a service ceiling of 24,000 ft (7,300 m).


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