- Specifications
- References
- External links
{{short description|Japanese airplane}}{{Expand Japanese|date=February 2016}}name = Kaishiki No.1 | image = File:会式一号機_sibling_of_Farman_III_(8237521286).jpg | caption = Replica at Tokorozawa Aviation Museum}{{Infobox Aircraft Type | type = First military airplane designed and flown in Japan | national origin=Japan | designer = Yoshitoshi Tokugawa | first flight = October 25, 1911 | primary user = | number built = 1 | unit cost = | developed from = Farman III | variants with their own articles = | developed into = Kaishiki No.2-6 }}{{Infobox aircraft career | other names = Kaishiki 1, Kaishiki Biplane 1 | type = Experimental biplane | manufacturer = | construction number = | construction date = | first flight = October 13, 1911 | last 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= }}
References1. ^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. ^1 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 |