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词条 Kaishiki No.1
释义

  1. Specifications

  2. References

  3. External links

{{short description|Japanese airplane}}{{Expand Japanese|date=February 2016}}
name = Kaishiki No.1image = File:会式一号機_sibling_of_Farman_III_(8237521286).jpgcaption = Replica at Tokorozawa Aviation Museum}{{Infobox Aircraft Typetype = First military airplane designed and flown in Japannational origin=Japandesigner = Yoshitoshi Tokugawafirst flight = October 25, 1911primary user =number built = 1unit cost =developed from = Farman IIIvariants with their own articles =developed into = Kaishiki No.2-6
}}{{Infobox aircraft career
other names = Kaishiki 1, Kaishiki Biplane 1type = Experimental biplanemanufacturer =construction number = construction date =first flight = October 13, 1911last flight =owners =in service = flights =total hours =total distance =aircraft carried = fate =preservation =
}}

The {{nihongo|会式一号機|Kaishiki No.1|kaishikiichigouki}} was the first successful{{#tag:ref|The civilian designed Narahara No. 2 made a {{convert|60|m|ft}} flight on 5 May 1911, but crashed on landing when its undercarriage failed.[1]|group=lower-alpha}} Japanese-designed and constructed airplane. It was designed by Captain Yoshitoshi Tokugawa and was first flown by him on October 13, 1911 at Tokorozawa in Saitama Prefecture.[1]

There is a replica displayed in the Tokorozawa Aviation Museum, located near the place where the aircraft's first flight took place.[2]

Specifications

{{Aircraft specs
|ref=Japanese Aircraft 1910–1941[3]
|prime units?=met


|genhide=
|crew=2
|capacity=
|length m=11.50
|length ft=
|length in=
|length note=
|span m=
|span ft=
|span in=
|span note=
|upper span m=10.50
|upper span ft=
|upper span in=
|upper span note=
|lower span m=8.0
|lower span ft=
|lower span in=
|lower span note=
|height m=3.90
|height ft=
|height in=
|height note=
|wing area sqm=41.0
|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=450
|empty weight lb=
|empty weight note=
|gross weight kg=550
|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=Gnome Omega
|eng1 type=7-cylinder rotary engine
|eng1 kw=
|eng1 hp=50
|eng1 note=
|prop blade number=2
|prop name=Chauvière
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=


|perfhide=
|max speed kmh=
|max speed mph=
|max speed kts=39
|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=
|endurance=3 hr
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=
|more performance=
|avionics=
}}

References

1. ^Tokorozawa Aviation Museum website Experience Exhibits {{webarchive|url=https://web.archive.org/web/20160314120633/http://tam-web.jsf.or.jp/contxe/modules/tinyd3/index.php?id=2 |date=2016-03-14 }} Retrieved February 13, 2016
2. ^Aviation Museum website Kaishiki 1 - Tokorozawa Aviation Museum Retrieved February 12, 2016
3. ^Mikesh and Abe 1990, p. 47.
{{reflist}}
  • {{cite book|last1=Mikesh|first1=Robert C.|last2=Abe|first2= Shorzoe |title=Japanese Aircraft 1910–1941 |year=1990 |publisher=Putnam Aeronautical Books|location=London| isbn=0-85177-840-2}}

External links

{{Commons}}

3 : Pusher aircraft|Rotary-engined aircraft|Biplanes

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