POTEZ 75
180 XLimits
7.6 years ago
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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.
Specifications
Spotlights
- AdamA 6.4 years ago
General Characteristics
- Created On Android
- Wingspan 37.1ft (11.3m)
- Length 29.9ft (9.1m)
- Height 10.3ft (3.1m)
- Empty Weight 4,747lbs (2,153kg)
- Loaded Weight 6,079lbs (2,757kg)
Performance
- Horse Power/Weight Ratio 0.164
- Wing Loading 25.9lbs/ft2 (126.2kg/m2)
- Wing Area 235.1ft2 (21.8m2)
- Drag Points 1831
Parts
- Number of Parts 43
- Control Surfaces 9
- Performance Cost 244