AC Mobil 34 Chrysalin
| Chrysalin | |
|---|---|
| Role | Microlight aircraft |
| National origin | France |
| Manufacturer | AC Mobil 34 |
| Status | In Production |
| Unit cost |
€45,750 (ready-to-fly, 2011)
|
The AC Mobil 34 Chrysalin is a two-seat light aircraft produced in France in kitplane form. The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules.[1]
Contents
Design and development
Constructed of composite materials, it is a conventional high-wing braced monoplane with fixed tricycle undercarriage. The pilot and passenger sit in side-by-side configuration.[1]
Construction is of fibreglass and vinylester sandwich, which results in a low empty weight of 283 kg (624 lb). The aircraft features folding wings. Standard engine is the 60 kW (80 hp) Rotax 912 air and liquid-cooled, four stroke, four cylinder piston aircraft engine.[1]
Specifications (Chrysalin)
General characteristics
- Crew: 1
- Capacity: 2
- Length: 6.2 m (20 ft 4 in)
- Wingspan: 9.6 m (31 ft 6 in)
- Height: 1.78 m (5 ft 10 in)
- Wing area: 13.6 m2 (146 sq ft)
- Empty weight: 268 kg (591 lb)
- Max takeoff weight: 450 kg (992 lb)
- Powerplant: 1 × Rotax 912 air-cooled, four stroke, four cylinder piston engine, 60 kW (80 hp)
Performance
- Maximum speed: 190 km/h (118 mph; 103 kn)
- Stall speed: 62 km/h (39 mph; 33 kn)
- Never exceed speed: 220 km/h (137 mph; 119 kn)
- Rate of climb: 5.25 m/s (1,033 ft/min)
- Wing loading: 33 kg/m2 (6.8 lb/sq ft)
Related content
Comparable aircraft:
References
<templatestyles src="Reflist/styles.css" />
Cite error: Invalid <references> tag; parameter "group" is allowed only.
<references />, or <references group="..." />External links
<templatestyles src="Asbox/styles.css"></templatestyles>
 |
This article on an aircraft of the 2000s is a stub. You can help Wikipedia by expanding it. |
