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词条 Caudron C.680
释义

  1. Design

  2. Specifications

  3. References

  4. Further reading

{{short description|1930s French aircraft}}
name = C.680image =caption =

}}{{Infobox Aircraft Type

type = Sports aircraftmanufacturer = Caudrondesigner =first flight = 1936introduced =retired =produced =number built = 1status =unit cost =primary user =more users =developed from =variants with their own articles =
}}

The Caudron C.680 was a 2-seat sport aircraft built by Caudron in the late 1930s.

Design

The C.680 was a low-wing monoplane of all-wood construction, with the airframe covered by canvas and plywood.

Specifications

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


|crew=2
|capacity=
|length m=7.07
|length ft=
|length in=
|length note=
|span m=7.7
|span ft=
|span in=
|span note=
|upper span m=
|upper span ft=
|upper span in=
|upper span note=
|mid span m=
|mid span ft=
|mid span in=
|mid span note=
|lower span m=
|lower span ft=
|lower span in=
|lower span note=
|swept m=
|swept ft=
|swept in=
|swept note=
|dia m=
|dia ft=
|dia in=
|dia note=
|width m=
|width ft=
|width in=
|width note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=9
|wing area sqft=
|wing area note=
|swept area sqm=
|swept area sqft=
|swept area note=
|volume m3=
|volume ft3=
|volume note=
|aspect ratio=
|airfoil=
|empty weight kg=
|empty weight lb=
|empty weight note=
|gross weight kg=
|gross weight lb=
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|lift kg=
|lift lb=
|lift note=
|more general=


|eng1 number=1
|eng1 name=Renault 4Pei
|eng1 type=4-cylinder inverted in-line piston engine
|eng1 kw=
|eng1 hp=140
|eng1 shp=
|eng1 kn=
|eng1 lbf=
|eng1 note=
|power original=
|thrust original=
|eng1 kn-ab=
|eng1 lbf-ab=
|eng2 number=
|eng2 name=
|eng2 type=
|eng2 kw=
|eng2 hp=
|eng2 shp=
|eng2 kn=
|eng2 lbf=
|eng2 note=
|eng2 kn-ab=
|eng2 lbf-ab=
|eng3 number=
|eng3 name=
|eng3 type=
|eng3 kw=
|eng3 hp=
|eng3 shp=
|eng3 kn=
|eng3 lbf=
|eng3 note=
|eng3 kn-ab=
|eng3 lbf-ab=
|more power=
|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=
|rot number=
|rot dia m=
|rot dia ft=
|rot dia in=
|rot area sqm=
|rot area sqft=
|rot area note=


|perfhide=
|max speed kmh=
|max speed mph=
|max speed kts=
|max speed note=
|max speed mach=
|cruise speed kmh=
|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=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|minimum control speed kmh=
|minimum control speed mph=
|minimum control speed kts=
|minimum control speed note=
|range km=
|range miles=
|range nmi=
|range note=
|combat range km=
|combat range miles=
|combat range nmi=
|combat range note=
|ferry range km=
|ferry range miles=
|ferry range nmi=
|ferry 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=
|disk loading kg/m2=
|disk loading lb/sqft=
|disk loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=
|thrust/weight=
|more performance=


|armament=


|guns=
|bombs=
|rockets=
|missiles=
|hardpoints=
|hardpoint capacity=
|hardpoint rockets=
|hardpoint missiles=
|hardpoint bombs=
|hardpoint other=
|avionics=
}}

References

1. ^{{cite web|url=https://www.aviafrance.com/caudron-c-680-aviation-france-9848.htm |title=Caudron C.680 - avion de sport - Un siècle d'aviation française |publisher=Aviafrance.com |date=2017-12-08 |accessdate=2019-01-29}}

Further reading

  • {{cite book |title=Les avions Caudron :Tome II |first1=Andre |last1=Hauet |publisher=Lela Presse |isbn=9782914017091}}
{{Caudron aircraft}}

4 : Caudron aircraft|Single-engined tractor aircraft|Low-wing aircraft|Aircraft first flown in 1936

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