Engineering:Pottier P.40
| Pottier P.40 | |
|---|---|
| |
| in the Royal Museum of the Armed Forces and Military History | |
| Role | Single seat tailless homebuilt sports aircraft |
| Designer | Jean Pottier |
| First flight | 1975 |
| Number built | 2 |
The France 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,[1] begun around 1967, though not the first to fly as the P.70 flew in August 1974.[2] Construction of the P.40 by Bela Nogrady was started in 1968 but the first flight was not made until 1975.[3]
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.[1]
The short fuselage is flat sided, mostly occupied by a long canopy over the single seat cockpit. The engine, a 19 kW (25 hp) Volkswagen 1.2 litre air-cooled flat-four, is in the rear in pusher configuration.[1] 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.[1][4] 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
Data from Gaillard (1991) p.150[1]
General characteristics
- Crew: One
- Length: 2.60 m (8 ft 6 in)
- Wingspan: 6 m (19 ft 8 in)
- Height: 1.20 m (3 ft 11 in)
- Wing area: 8 m2 (86 sq ft)
- Empty weight: 150 kg (331 lb)
- Max takeoff weight: 270 kg (595 lb)
- Powerplant: 1 × Volkswagen 1.2 litre air-cooled flat-four, 19 kW (25 hp)
- Propellers: 2 (3 on second aircraft)-bladed
Performance
- Maximum speed: 180 km/h (110 mph, 97 kn)
- Cruise speed: 160 km/h (99 mph, 86 kn)
- Range: 600 km (370 mi, 320 nmi)
- Service ceiling: 2,900 m (9,500 ft) [3]
References
- ↑ 1.0 1.1 1.2 1.3 1.4 Gaillard, Pierre (1991). Les Avions Francais de 1965 à 1990. Paris: Éditions EPA. pp. 150. ISBN 2-85120-392-4.
- ↑ Gaillard (1991). Les Avions Francais de 1965 à 1990. Éditions EPA. pp. 130.
- ↑ 3.0 3.1 Walter van Tilborg. "Poittier P.40 (OO-68)". http://1000aircraftphotos.com/Contributions/Hodgson/8569.htm.
- ↑ Chillon, Jacques. Fox Papa - Registre des avions Français amateur (2009 ed.). Brive: Ver Luisant. p. 162. ISBN 978-2-3555-1-066-3.
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