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・ Focke-Wulf Fw 206
・ Focke-Wulf Fw 260
・ Focke-Wulf Fw 300
・ Focke-Wulf Fw 42
・ Focke-Wulf Fw 43
・ Focke-Wulf Fw 44
・ Focke-Wulf Fw 47
・ Focke-Wulf Fw 56
・ Focke-Wulf Fw 57
・ Focke-Wulf Fw 58
・ Focke-Wulf Fw 61
・ Focke-Wulf Fw 62
・ Focke-Wulf GL 18
・ Focke-Wulf Project I
・ Focke-Wulf Project II
Focke-Wulf Project III
・ Focke-Wulf Project VIII
・ Focke-Wulf S 2
・ Focke-Wulf S 24
・ Focke-Wulf Super Lorin
・ Focke-Wulf Ta 152
・ Focke-Wulf Ta 153
・ Focke-Wulf Ta 154
・ Focke-Wulf Ta 183
・ Focke-Wulf Ta 254
・ Focke-Wulf Ta 283
・ Focke-Wulf Ta 400
・ Focke-Wulf Triebflügel
・ Focke-Wulf Volksjäger
・ Fockea


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Focke-Wulf Project III : ウィキペディア英語版
Focke-Wulf Project III
__NOTOC__

The Focke-Wulf Project III was a design study for a jet fighter carried out in Germany in June 1943. It aimed to reduce the risk of foreign object damage to the engine that had been foreseen for the Project II by relocating the engine from beneath the fuselage to a position atop the fuselage, with the jet intakes at the fuselage sides. In most other respects, it was similar to Project II, but as well as the engine relocation, Project II's conventional tail was replaced with twin tails on the ends of the horizontal stabiliser, in order to provide a path for the jet exhaust.
Project IV was to be virtually identical, but included a liquid-fuelled rocket booster on each side of the turbojet nacelle.






==See also==

*Emergency Fighter Program

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
ウィキペディアで「Focke-Wulf Project III」の詳細全文を読む



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