关于FB-111A的有些问题的请教

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有资料上说FB-111A是用F-111A的机身和B的机翼组合而成的,所以长度和F-111A一样,都是22.4米,但又有资料说FB-111A为了加载更多内油,实际长度相比F-111A长了两英尺。请问到底是什么情况,还有FB-111A和F-111A在外型上,初了引擎,机翼,起落架还有什么不同吗?谢谢有资料上说FB-111A是用F-111A的机身和B的机翼组合而成的,所以长度和F-111A一样,都是22.4米,但又有资料说FB-111A为了加载更多内油,实际长度相比F-111A长了两英尺。请问到底是什么情况,还有FB-111A和F-111A在外型上,初了引擎,机翼,起落架还有什么不同吗?谢谢
自顶一下


Joseph F. Baugher :

FB-111A strategic bomber
The FB-111A was the all-weather strategic bombing version of the F-111, intended as an interim successor to the B-52 and B-58 of the Strategic Air Command. It was initially developed as Weapon System 129A.

The FB-111A differed from the F-111A primarily in having a longer fuselage (75 feet 7 inches as compared to 73 feet 5 1/2 inches) to accommodate the additional fuel required for its strategic mission. In order to provide a longer range and greater load-lifting capability, the FB-111A had the extended wing of the F-111B (unfolded span of 70 feet as compared to 63 feet). It also had a stronger undercarriage and landing gear, and was powered by TF30-P-7 turbofan engines. It featured the Mark IIB avionic subsystem planned for the F-111E, which comprised an improved F-111A attack radar, an inertial navigation system, digital computers, plus some advanced displays of the later Mark II that equipped the delayed F-111D



另外如果和F-111A比的话,

FB-111A用的是Triple Plow II 进气口(可调式进气锥没有巨大的附面层隔板)

F-111A是TP I

Joseph F. Baugher :

FB-111A strategic bomber
The FB-111A was the all-weather strategic bombing version of the F-111, intended as an interim successor to the B-52 and B-58 of the Strategic Air Command. It was initially developed as Weapon System 129A.

The FB-111A differed from the F-111A primarily in having a longer fuselage (75 feet 7 inches as compared to 73 feet 5 1/2 inches) to accommodate the additional fuel required for its strategic mission. In order to provide a longer range and greater load-lifting capability, the FB-111A had the extended wing of the F-111B (unfolded span of 70 feet as compared to 63 feet). It also had a stronger undercarriage and landing gear, and was powered by TF30-P-7 turbofan engines. It featured the Mark IIB avionic subsystem planned for the F-111E, which comprised an improved F-111A attack radar, an inertial navigation system, digital computers, plus some advanced displays of the later Mark II that equipped the delayed F-111D



另外如果和F-111A比的话,

FB-111A用的是Triple Plow II 进气口(可调式进气锥没有巨大的附面层隔板)

F-111A是TP I