Engineering:AC Mobil 34 Chrysalin
From HandWiki
| Chrysalin | |
|---|---|
| Role | Microlight aircraft |
| National origin | France |
| Manufacturer | AC Mobil 34 |
| Status | In Production |
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][2]
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][2]
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][2]
Specifications (Chrysalin)
Data from Tacke[2]
General characteristics
- Crew: one
- Capacity: one passenger
- Wingspan: 9.6 m (31 ft 6 in)
- Wing area: 13.5 m2 (145 sq ft)
- Aspect ratio: 6.83
- Empty weight: 283 kg (624 lb)
- Max takeoff weight: 472.5 kg (1,042 lb)
- Powerplant: 1 × Rotax 912 air-cooled, four stroke, four cylinder piston engine, 60 kW (80 hp)
Performance
- Maximum speed: 190 km/h (120 mph, 100 kn)
- Cruise speed: 150 km/h (93 mph, 81 kn)
- Stall speed: 62 km/h (39 mph, 33 kn)
- Rate of climb: 5.25 m/s (1,033 ft/min)
See also
Comparable aircraft:
References
- ↑ 1.0 1.1 1.2 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011–12, page 12. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
- ↑ 2.0 2.1 2.2 2.3 Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015–16, page 12. Flying Pages Europe SARL, 2015. ISSN 1368-485X
External links
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