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词条 Naval Air Establishment Chiang Hung
释义

  1. Operators

  2. Specifications

  3. References

  4. Further reading

name=Chiang Hungimage=caption=

}}{{Infobox Aircraft Type

type=Reconnaissance seaplanemanufacturer=Naval Air Establishmentdesigner=first flight=introduced=retired=status=primary user=Chinese Navymore users=produced=number built=2variants with their own articles=
}}

The Naval Air Establishment Chiang Hung (江鴻 - "River Swan") was a reconnaissance seaplane developed for the Chinese Navy in the late 1920s. It was a conventional biplane design with single-bay, unstaggered wings of equal span and accommodation for the pilot and observer in tandem, open cockpits. The landing gear consisted of twin pontoons.

Operators

{{China as ROC}}
  • Chinese Navy

Specifications

{{Aircraft specs
|ref=A History of Chinese Aviation[1], Jane's all the World's Aircraft 1931[2]
|prime units?=met


|crew=2
|length m=8.33
|upper span m=10.54
|lower span m=10.88
|height m=3.56
|wing area sqm=31.4
|aspect ratio=
|airfoil=
|empty weight kg=740
|gross weight kg=1180
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=


|eng1 number=1
|eng1 name=Wright J-5 Whirlwind
|eng1 type=5-cylinder air-cooled radial piston engine
|eng1 hp=165
|prop blade number=2
|prop name=wooden fixed-pitch propeller
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=


|perfhide=
|max speed kmh=177
|max speed note=

  • Alighting speed: {{cvt|85|km/h|mph kn}}

|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=
|range miles=
|range nmi=
|range note=
|ferry range km=
|ferry range miles=
|ferry range nmi=
|ferry range note=
|endurance=
|ceiling ft=15500
|ceiling note=Absolute ceiling
|g limits=
|roll rate=
|glide ratio=
|climb rate ftmin=514
|time to altitude={{cvt|3050|m}} in 31 minutes
|wing loading kg/m2=37.6
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass={{cvt|15.75|lb/hp|kg/kW|order=flip}}
|more performance=
}}

References

1. ^{{cite book|last=Andersson|first=Lennart|title=A History of Chinese Aviation: Encyclopedia of Aircraft and Aviation in China until 1949|year=2008|publisher=AHS of ROC|location=Taipei, Republic of China|isbn=978-957-28533-3-7 |page=238}}
2. ^{{cite book |title=Jane's all the World's Aircraft 1931 |editor1-last=Grey |editor1-first=C.G. |year=1928 |publisher=Sampson Low, Marston & company, ltd |location=London |page=88c}}

Further reading

  • {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London |pages=254 }}
  • {{cite book |title=Jane's all the World's Aircraft 1933 |editor1-last=Grey |editor1-first=C.G. |year=1933 |publisher=Sampson Low, Marston & company, ltd |location=London |page=86c}}
{{Aircraft manufacturers of China}}

5 : Chinese military reconnaissance aircraft 1920–1929|Floatplanes|Biplanes|Single-engined tractor aircraft|Naval Air Establishment aircraft

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