Pottier P.40
| {{Infobox Aircraft Begin
| name=Pottier P.40 | image=RMM Brussel Pottier P40.JPG | caption=in the Royal Museum of the Armed Forces and Military History }}{{Infobox Aircraft Type | type=Single seat tailless homebuilt sports aircraft | national origin= | manufacturer= | designer=Jean Pottier | first flight=1975 | introduced= | retired= | status= | primary user= | more users= | produced= | number built= 2 | program cost= | unit cost= | developed from= | variants with their own articles= }} |
The French tailless Pottier P.40 was the first aircraft designed by Jean Pottier. It flew in 1975.
Design
The Pottier P.40 was the first of Jean Pottier's many designs, begun around 1967, though not the first to fly as the P.70 flew in August 1974. Construction of the P.40 by Bela Nogrady was started in 1968 but the first flight was not made until 1975.
The P.40 is a tailless aircraft with a swept, cantilever, low wing. In plan, the wing has a rectangular centre section and straight tapered outer panels with elevons. There are wing tip fins and outward opening rudders which extend a little below the wing.
The short fuselage is flat sided, mostly occupied by a long canopy over the single seat cockpit. The engine, a {{convert|25|hp|kW|abbr=on|0|order=flip}} Volkswagen 1.2 litre air-cooled flat-four, is in the rear in pusher configuration. The P.40 has a low, fixed, faired bicycle undercarriage.
Operational history
The first P.40 made only one short flight and was then destroyed. The history of the one surviving example, OO-68, on display in the Belgian Royal Museum of the Armed Forces and Military History in Brussels is obscure. The two machines differed a little, with varying engine cooling and exhaust arrangements, and OO-68 has a three, rather than two, blade propeller.
Specifications
{{Aircraft specs
|prime units?=met
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|crew=One
|length m=2.60
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|span m=6
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|height m=1.20
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|wing area sqm=8
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|empty weight kg=150
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|max takeoff weight kg=270
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|eng1 number=1
|eng1 name=Volkswagen 1.2 litre
|eng1 type=air-cooled flat-four
|eng1 hp=25
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|prop blade number=2 (3 on second aircraft)
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|max speed kmh=180
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|cruise speed kmh=160
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|range km=600
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|ceiling m=2900
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References
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{{Pottier aircraft}}
Category:Single-engined pusher aircraft