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P-75
Eagle
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Photo: Robert Deering 10/18/2012
National Museum of the USAF
Wright-Paterson AFB (FFO)
Dayton, Ohio
The Fisher P-75 Eagle was intended to fill the Army Air Forces' 1942 need for an interceptor. Its unique design featured two coaxial contra-rotating propellers connected by dual drive shafts running under the cockpit to a 24-cylinder, liquid-cooled engine located amidships. The original concept called for use of proven airframe components such as P-40 wing panels, A-24 tail, and F4U landing gear--to reduce the design and testing period.

The first of two XP-75s using component parts made its initial flight on Nov. 17, 1943. Flight tests revealed unsatisfactory performance. This, combined with a mission change from interceptor to long-range escort, caused major changes in the original design. Ultimately, the idea of using proven airframe components had to be abandoned. The AAF ordered six XP-75s of the revised configuration along with 2,500 P-75As. The improved version was still unsatisfactory and after three Eagles had crashed, the entire program was canceled on Nov. 8, 1944. Only eight XP-75s and six P-75As were built.
SPECIFICATIONS: (P-75A): PERFORMANCE:
Span:  49 ft. 4 in. Maximum speed:  404 mph
Length:  40 ft. 5 in. Cruising speed:  250 mph
Height:  15 ft. 6 in. Range:  2,600 mi.
Empty Weight:  Service ceiling:  36,400 ft.
Gross Weight:  19,420 lbs. loaded  
Crew:  One
Engines:  Allison V-3420 of 2,885 hp
Armament:  10 .50 cal. machine guns and two 500-lb. bombs
   
SOURCE:  National Museum of the United States Air Force