| DC.1 | |
|---|---|
| Role | Ultralight monoplane |
| National origin | France |
| Manufacturer | Délémontez-Cauchy |
| Designer | Jean Délémontez |
| First flight | July 6, 1980 |
| Developed from | Jodel D.9 |
The Délémontez-Cauchy DC.1 is a French ultralight monoplane designed by Jean Délémontez for amateur construction, derived from the Jodel D.9.
Specifications
Data from Les Avions Français de 1965 a 1990[1]
General characteristics
- Crew: 2
- Length: 5.65 m (18 ft 6 in)
- Wingspan: 7.4 m (24 ft 3 in)
- Wing area: 9.56 m2 (102.9 sq ft)
- Empty weight: 225 kg (496 lb)
- Gross weight: 397 kg (875 lb)
- Powerplant: 1 × Volkswagen 1,600 cm3 (98 cu in) conversion 4-cylinder air-cooled horizontally-opposed piston engine, 48 kW (65 hp)
- Propellers: 2-bladed fixed-pitch propeller
Performance
- Maximum speed: 194 km/h (121 mph, 105 kn)
- Cruise speed: 175 km/h (109 mph, 94 kn)
- Economical cruise speed: 140 km/h (87 mph; 76 kn)
References
- ^ Gaillard, Pierre (1991). Les avions français de 1965 a 1990 (in French). Paris: EPA Editions. p. 175. ISBN 2851203924.
External links
- Parmentier, Bruno (8 December 2017). "Délémontez-Cauchy DC.1". Aviafrance (in French). Paris. Retrieved 8 March 2019.
 | This aircraft-related article is a stub. You can help Wikipedia by expanding it. |
This page was last edited on 25 January 2022, at 21:36