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词条 Cukurs C.6bis
释义

  1. Development

  2. Specifications (C.6bis)

  3. References

name =Cukurs C.6bisimage =Cukurs C-6bis.jpgcaption =

}}{{Infobox Aircraft Type

type = Dive bombermanufacturer = Herberts Cukursdesigner =Herberts Cukursfirst flight = 1940introduced = 1940retired =status =primary user =Latvian Air Forcemore users =produced =number built = 1unit cost =variants with their own articles =
}}
Cukurs C.6bis was a Latvian prototype dive bomber aircraft designed by Herberts Cukurs in 1940.[1]

Development

The aircraft was based on the Cukurs C.6 Trīs zvaigznes (Three stars) trainer which was known for its 1937 flight from Riga to Tokyo and return.[1]

Work on the C.6bis started in 1939, with the first test flights in 1940. Soon after first test flights the Latvian Air Force accepted the aircraft and ordered twelve.[1]

Test flights were halted on the 7 June 1940, just 10 days before the Soviet occupation of Latvia in 1940. During the occupation the Red Army expressed interest in the C.6bis and test flew it, but they determined that it was unsuitable for use.{{Citation needed|date=April 2012}}

Only one example was built and its fate remains unknown.{{Citation needed|date=April 2012}}

Specifications (C.6bis)

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


|genhide=
|crew=two
|capacity=
|length m=8.50
|length ft=
|length in=
|length note=
|span m=11.00
|span ft=
|span in=
|span note=
|height m=2.40
|height ft=
|height in=
|height note=
|wing area sqm=12.80
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=680
|empty weight lb=
|empty weight note=
|gross weight kg=
|gross weight lb=
|gross weight note=
|max takeoff weight kg=1340
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=


|eng1 number=1
|eng1 name=Hispano Suiza 6 Mb
|eng1 type=six cylinder liquid-cooled in-line piston aircraft engine
|eng1 kw=
|eng1 hp=280
|eng1 shp=
|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=


|perfhide=
|max speed kmh=440
|max speed mph=
|max speed kts=
|max speed note=
|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=
|range km=680
|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=5800
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=
|thrust/weight=
|more performance=


|guns=
|bombs= 50 kg each
|rockets=
|missiles=
|hardpoints=
|hardpoint capacity=
|hardpoint rockets=
|hardpoint missiles=
|hardpoint bombs=
|hardpoint other=
|avionics=
}}

References

1. ^{{cite web|url=http://www.airwar.ru/enc/other2/c6bis.html |title=Cukurs C-6bis |publisher=Airwar.ru |date= |accessdate=2012-04-28}}

2 : Aircraft manufactured in Latvia|Latvian bomber aircraft 1930–1939

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