- Mirage Celerity
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Celerity Role Homebuilt light aircraft National origin United States Manufacturer Mirage Aircraft Designer Larry Burton First flight 18 May 1985 The Mirage Celerity is an American two-seat cabin monoplane designed by Larry Burton and with plans for home building sold by Mirage Aircraft of Tucson AZ, United States.[1]
Design and development
The Celerity is a side-by-side two-seat low-wing cabin monoplane built from a mixture of composites and wood.[1] Nominally powered by a 160 hp (119 kW) Lycoming O-320-B1A piston engine and with a retractable conventional landing gear.[1]
Specifications
Data from [1]Brassey's World Aircraft & Systems Directory
General characteristics
- Crew: 2
- Length: 21 ft 6 in (6.55 m)
- Wingspan: 23 ft 10 in (7.26 m)
- Empty weight: 1169 lb (530 kg)
- Gross weight: 1825 lb (828 kg)
- Powerplant: 1 × Lycoming O-320-B1A, 160 hp (119 kW)
Performance
- Maximum speed: 220 mph (354 km/h)
- Stall speed: 53 mph (86 km/h)
- Range: 1000 miles (1609 km)
- Rate of climb: 1800 ft/min (549 m/s)
References
Notes
Bibliography
- Taylor, Michael J. H. (1996). Brassey's World Aircraft & Systems Directory. London, England: Brassey's. ISBN 1 85733 1981 1.
External links
Lists relating to aviation General Aircraft (manufacturers) · Aircraft engines (manufacturers) · Airlines (defunct) · Airports · Civil authorities · Museums · Registration prefixes · Rotorcraft (manufacturers) · TimelineMilitary Accidents/incidents Records Categories:- United States civil utility aircraft 1980–1989
- Homebuilt aircraft
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