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General Electric CJ805
The General Electric CJ805 is a jet engine which was developed by GE Aviation in the late 1950s. A simplified civilian version of the J79 featuring an axial compressor, it was developed in two versions. The basic CJ805-3 was a turbojet and powered the Convair 880, while CJ805-23 (military designation TF35), a turbofan derivative, powered the Convair 990 airliners.
==Variants and applications==
;CJ805-3:Convair 880
;CJ805-3A:Convair 880-22 : Revised variable inlet guide vane and stator control.〔
;CJ805-3B:Convair 880-22M : Increased thrust.〔
;CJ805-23:Flight testing in a Douglas RB-66: Aft-fan variant with a direct drive fan attached to a free-running LP turbine.〔
;CJ805-23A:〔
;CJ805-23B:Convair 990〔
;CJ805-23C:Intended for the proposed Sud Aviation Caravelle 10A〔
Only a single Sud Aviation Caravelle intended as a prototype for the US market, was equipped with the CJ805.
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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