avia.wikisort.org - Aeroplane
The Fly Synthesis Catalina NG is an Italian ultralight and light-sport amphibious flying boat, designed and produced by Fly Synthesis, introduced at the Aero show held in Friedrichshafen in 2010. The aircraft is supplied as a complete ready-to-fly-aircraft.[1][2]
| Catalina | |
|---|---|
 | |
| Role | Ultralight and light-sport amphibious flying boat |
| National origin | Italy |
| Manufacturer | Fly Synthesis |
| Introduction | 2010 |
| Status | In production |
Design and development
The manufacturer says the design borrowed from the development of the earlier Fly Synthesis Storch, stating, "The Catalina NG project evolved from the Storch amphibious aircraft experience".[3]
The Catalina was designed to comply with the Fédération Aéronautique Internationale microlight rules and US light-sport aircraft rules. It features a strut-braced high-wing, a two-seats-in-side-by-side configuration open cockpit, electrically retractable tricycle landing gear and a single engine in tractor configuration.[1][2]
The aircraft is made from composite material, predominantly carbon fibre and fibreglass. Its 9.47 m (31.1 ft) span wing has an area of 12.6 m2 (136 sq ft) and electrically-operated flaperons. The standard engine available is the 64 hp (48 kW) Rotax 582 two-stroke powerplant. Folding wings and a ballistic parachute are optional equipment.[1][2][3]
Specifications (Catalina NG)
Data from Manufacturer and Bayerl[1][3]
General characteristics
- Crew: one
- Capacity: one passenger
- Length: 6.28 m (20 ft 7 in)
- Wingspan: 9.47 m (31 ft 1 in)
- Height: 2.49 m (8 ft 2 in)
- Wing area: 12.6 m2 (136 sq ft)
- Empty weight: 292 kg (644 lb)
- Gross weight: 495 kg (1,091 lb)
- Fuel capacity: 50 litres (11 imp gal; 13 US gal) in two 25 litres (5.5 imp gal; 6.6 US gal) tanks
- Powerplant: 1 × Rotax 582 twin cylinder, liquid-cooled, two stroke aircraft engine, 48 kW (64 hp)
Performance
- Cruise speed: 125 km/h (78 mph, 67 kn)
- Stall speed: 60 km/h (37 mph, 32 kn)
- Never exceed speed: 150 km/h (93 mph, 81 kn)
- g limits: +4/-2
- Rate of climb: 4.5 m/s (890 ft/min)
- Wing loading: 39.3 kg/m2 (8.0 lb/sq ft)
References
- Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 52. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
- Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 54. Flying Pages Europe SARL, 2015. ISSN 1368-485X
- Fly Synthesis (2011). "Catalina NG - Technical data". Archived from the original on 13 January 2012. Retrieved 20 June 2012.
External links
Другой контент может иметь иную лицензию. Перед использованием материалов сайта WikiSort.org внимательно изучите правила лицензирования конкретных элементов наполнения сайта.
WikiSort.org - проект по пересортировке и дополнению контента Википедии