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・ Potez 452
・ Potez 4D
・ Potez 4E
・ Potez 506
・ Potez 53
・ Potez 540
・ Potez 56
・ Potez 58
・ Potez 60
・ Potez 62
・ Potez 630
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・ Potez 661
・ Potez 662
・ Potez 6D
Potez 75
・ Potez 840
・ Potez 8D
・ Potez IX
・ Potez SEA VII
・ Potez VIII
・ Potez X
・ Potez XI
・ Potez XVIII
・ Potez-CAMS 141
・ Potez-CAMS 160
・ Potez-CAMS 161
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Potez 75 : ウィキペディア英語版
Potez 75
The Potez 75 was a French light ground attack pusher configuration monoplane of the 1950s.
==Design and development==

The Potez 75 was developed by the reformed Potez Company which had originally been formed by Henry Potez in 1919. The type was designed to meet the requirement for a launching platform for wire-guided anti-tank missiles Nord SS.10. It was of all-metal construction, with a pusher engine. The twin fins and tailplane were carried on two booms extending from the lower rear fuselage and it was fitted with a fixed tricycle undercarriage. The missile operator sat in the nose, behind which was a small upper cabin accommodating the pilot. Initially the operator's cabin had windows and the pilot's position was open, but later modifications enclosed the latter and provided the operator with better visibility by full glazing.

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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