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词条 Corvus Racer 312
释义

  1. Design and development

  2. Specifications (Racer 312)

  3. References

  4. External links

name= Racer 312 image= caption=

}}{{Infobox Aircraft Type

type=Ultralight aircraft and Light-sport aircraft national origin=China manufacturer=Corvus Aerospace (Suzhou) designer= first flight=1 November 2013 introduced= retired= status=Under development (2015) primary user= more users= produced= number built= program cost= unit cost= developed from= variants with their own articles=
}}

The Corvus Racer 312 is a Chinese ultralight and light-sport aircraft under development by Corvus Aerospace (Suzhou) of Suzhou and first flown 1 November 2013. The aircraft is to be supplied complete and ready-to-fly.[1]

Design and development

The Racer 312 was designed as a smaller version of the Corvus Racer 540, to comply with the Fédération Aéronautique Internationale microlight rules and US light-sport aircraft rules. It was designed and the prototype built over a period of 13 months in 2012-13.[1]

The Racer 312 features a cantilever low-wing, two-seats-in-side-by-side configuration under a bubble canopy, fixed tricycle landing gear and a single engine in tractor configuration. The aircraft is made from composite material and its {{convert|8.33|m|ft|1|abbr=on}} span wing employs split flaps. The standard engine fitted is the {{convert|100|hp|kW|0|abbr=on}} Rotax 912ULS four-stroke powerplant. With this engine the cruise speed is anticipated to be {{convert|280|km/h|mph|0|abbr=on}}.[1]

As of February 2017, the design does not appear on the Federal Aviation Administration's list of approved special light-sport aircraft.[2]

Specifications (Racer 312)

{{Aircraft specs
|ref=Tacke[1]
|prime units?=met


|genhide=
|crew=one
|capacity=one passenger
|length m=
|length ft=
|length in=
|length note=
|span m=8.33
|span ft=
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=295
|empty weight lb=
|empty weight note=
|gross weight kg=472.5
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|108|l}}
|more general=


|eng1 number=1
|eng1 name=Rotax 912ULS
|eng1 type=four cylinder, liquid and air-cooled, four stroke aircraft engine
|eng1 kw=75
|eng1 hp=
|prop blade number=3
|prop name=composite
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=


|perfhide=
|max speed kmh=
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=280
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=340
|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=
|roll rate=
|glide ratio=
|climb rate ms=
|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=
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}

References

1. ^Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 40. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}
2. ^{{cite web|url = https://www.faa.gov/aircraft/gen_av/light_sport/media/SLSA_Directory.xlsx|title = SLSA Make/Model Directory|accessdate = 3 February 2017|last = Federal Aviation Administration|date = 26 September 2016}}

External links

  • {{Official website|http://www.corvus-china.com/}}
{{Corvus Aircraft}}

4 : Corvus aircraft|Chinese ultralight aircraft 2010–2019|Light-sport aircraft|Single-engined tractor aircraft

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