Payen AP.10
The Payen AP.10 was an experimental aircraft designed by Nicolas Payen in the 1930s.
| Payen AP.10 | |
|---|---|
 | |
| Role | Experimental aircraft |
| National origin | France |
| Manufacturer | Payen |
| First flight | 1936 |
| Number built | 1 |
Design
The AP.10 was a single-seat aircraft that was notable for the lack of a horizontal stabilizer.
Specifications
Data from [1]
General characteristics
- Crew: 1
- Length: 4.16 m (13 ft 8 in)
- Wingspan: 4.95 m (16 ft 3 in)
- Height: 1.86 m (6 ft 1 in)
- Wing area: 10.00 m2 (107.6 sq ft)
- Empty weight: 200 kg (441 lb)
- Gross weight: 340 kg (750 lb)
- Powerplant: 1 × Train inverted air-cooled in-line piston engine, 30 kW (40 hp)
Performance
- Maximum speed: 200 km/h (120 mph, 110 kn)
- Range: 900 km (560 mi, 490 nmi)
- Service ceiling: 5,000 m (16,000 ft)
References
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Wikimedia Commons has media related to Payen AP.10. |
- "Payen AP.10". Aviafrance.com. Retrieved 8 February 2019.
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