“Fly Synthesis Catalina”的意思、由来-开放百科全书

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Fly Synthesis Catalina

释义

Design and development
Specifications (Catalina NG)
References
External links

name=Catalina

image=Fly Synthesis Catalina at AERO Friedrichshafen 2018, Friedrichshafen (1X7A4291).jpg

caption=

}}{{Infobox Aircraft Type

type=Ultralight and light-sport amphibious flying boat

national origin=Italy

manufacturer=Fly Synthesis

designer=

first flight=

introduced=2010

retired=

status=In production

primary user=

more users=

produced=

number built=

program cost=

unit cost= €38,000 (2015)

developed from=

variants with their own articles=
}}

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]

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, predominately carbon fibre and fibreglass. Its {{convert|9.47|m|ft|1|abbr=on}} span wing has an area of {{convert|12.6|m2|sqft|abbr=on}} and electrically-operated flaperons. The standard engine available is the {{convert|64|hp|kW|0|abbr=on}} Rotax 582 two-stroke powerplant. Folding wings and a ballistic parachute are optional equipment.^[1]^[2]^[3]

Specifications (Catalina NG)

{{Aircraft specs
|ref=Manufacturer and Bayerl^[1]^[3]
|prime units?=met

|genhide=
|crew=one
|capacity=one passenger
|length m=6.28
|length ft=
|length in=
|length note=
|span m=9.47
|span ft=
|span in=
|span note=
|height m=2.49
|height ft=
|height in=
|height note=
|wing area sqm=12.6
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=292
|empty weight lb=
|empty weight note=
|gross weight kg=495
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|50|l}} in two {{convert|25|l}} tanks
|more general=

|perfhide=
|max speed kmh=
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=125
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=60
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=150
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|range km=
|range miles=
|range nmi=
|range note=
|endurance=
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=+4/-2
|roll rate=
|glide ratio=
|climb rate ms=4.5
|climb rate ftmin=
|climb rate note=
|time to altitude=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=39.3
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}

References

1. ^¹²³Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 52. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
2. ^¹²Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 54. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}
3. ^¹²{{cite web|url = http://www.flysynthesis.com/en/aerei/page88/catalina.html|title = Catalina NG - Technical data|accessdate = 20 June 2012|last = Fly Synthesis|year = 2011|archiveurl = https://web.archive.org/web/20120113153008/http://www.flysynthesis.com/en/aerei/page88/catalina.html |archivedate = 13 January 2012}}

External links

{{Official website|http://www.flysynthesis.com/aerei/catalina/catalina.html}}

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