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Consolidated Vultee XP-81
The Consolidated Vultee XP-81 (later redesignated ZXF-81) was a development of the Consolidated Vultee Aircraft Corporation to build a single seat, long range escort fighter that combined use of both turbojet and turboprop engines. Although promising, the lack of a suitable engine combined with the end of World War II doomed the project.
==Design and development==
Two prototype aircraft were ordered on 11 February 1944 that were designated XP-81. The engine selection was an attempt to couple the high-speed capability of the jet engine with the endurance offered by the propeller engine. The XP-81 was designed to use the General Electric TG-100 turboprop engine (later designated XT31 by the US military) in the nose driving a four-bladed propeller and an GE J33 turbojet in the rear fuselage. The turboprop would be used for normal flight and cruising and the turbojet added for high-speed flight.
抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』
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