Engineering:Délémontez-Desjardins D.01
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Revision as of 16:22, 6 April 2022 by imported>SpringEdit (add)
Short description: 1980s French aircraft
| D.01 Ibis | |
|---|---|
| Role | Ultralight monoplane |
| National origin | France |
| Manufacturer | Jacques Desjardins |
| Designer | Jean Délémontez |
| First flight | 12 June 1985 |
| Developed from | Jodel D.11 |
The Délémontez-Desjardins D.01 'Ibis' is a French ultralight monoplane designed by Jean Délémontez for amateur construction, derived from the Jodel D.11.
Specifications
Data from Les Avions Français de 1965 a 1990[1]
General characteristics
- Crew: 1 or 2
- Capacity: 1 or 2 pax
- Length: 6.3 m (20 ft 8 in)
- Wingspan: 8.22 m (27 ft 0 in)
- Wing area: 12.75 m2 (137.2 sq ft)
- Empty weight: 357 kg (787 lb)
- Gross weight: 617 kg (1,360 lb)
- Powerplant: 1 × Lycoming O-235 4-cylinder air-cooled horizontally-opposed piston engine, 75 kW (100 hp)
- Propellers: 2-bladed variable-pitch propeller
Performance
- Maximum speed: 200 km/h (120 mph, 110 kn)
- Cruise speed: 185 km/h (115 mph, 100 kn)
- Endurance: 3 hours
- Service ceiling: 4,000 m (13,000 ft)
References
- ↑ Gaillard, Pierre (1991) (in fr). Les avions français de 1965 a 1990. Paris: EPA Editions. p. 220. ISBN 2851203924.
External links
- Parmentier, Bruno (8 December 2017). "Délémontez-Desjardins D.01 'Ibis'" (in fr). Paris. https://www.aviafrance.com/aviafrance1.php?ID=9060&ID_CONSTRUCTEUR=417&ANNEE=0&ID_MISSION=0&MOTCLEF=. Retrieved 8 March 2019.
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