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North American F-82 Twin Mustang



 
Once the standard long-range, high-altitude escort fighter for the U.S. Air Force, the North American P-82 Twin Mustang was the climactic development of a long series of the famous World War II P-51 Mustang series. First flight of P-82 was on June 16, 1945. After 1947, the old P for Pursuit designation was replaced by F for Fighter, so the aircraft became known as the F-82.
North American produced 250 of the double-fuselaged airplanes for the Air Force, embracing three versions of the Twin Mustang then in service, the P-82E, P-82F, and P-82G. They were ordered too late for World War II, however.
The versatility of the P-82 made it potentially adaptable to a wide variety of roles in modern aerial warfare. It could have been used as a fighter, a long-range escort (of B-29 bombers), long-range reconnaissance, night fighter, attack bomber, rocket fighter or an interceptor.
With a speed of more than 475 miles an hour, the Twin Mustang had a combat range of over 1,600 miles with full armament. Range could be extended by use of external drop tanks on the wings.
A radical departure from the conventional single-fuselage airplane, the Twin Mustang was formed by two fuselages joined by the wing and the horizontal stabilizer. With a pilot in each fuselage, it reduced to a minimum the problem of pilot fatigue on ultra-long-range missions. The P-82F and G models carried a radar operator in the right cockpit instead of a co-pilot.
Both engine throttles and both propellers were controllable from either cockpit by manually operated levers. The pilot's  cockpit on the left contained the normal flight and engine instruments, while the co-pilot on the right had sufficient instruments for relief and emergency operation.
A simplified cockpit arrangement improved pilot comfort, including a tilting, adjustable seat to reduce fatigue during long flights.
General characteristics
Primary function Long range fighter
Power plant Two Packard Merlin V-1650-19/21 engines (in P-82B only, all other models used Allison V-1710s) liquid-cooled supercharged V-12 inline.
Thrust 2x 1,600 HP 2x 1,193 kW
Length 42 ft 5 in 12.93 m
Height 13 ft 10 in 4.22 m
Wingspan 51 ft 3 in 15.62 m
Wingarea 408 sq ft 37.9 sq m
Weight empty 15,997 lb 7,256 kg
max. takeoff 25,591 lb 11,608 kg
Range 2,240 miles 3,605 km
Speed cruising 286 mph 460 km/h
maximum 461 mph 762 km/h
Ceiling 38,900 ft 11,855 m
Armament Six .50 caliber machine guns; up to 4,000 lb of bombs
Crew Two (pilot, copilot/radar operator)


Jirka Wagner

 

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Last updated 01.01.2017