| 词条 | Korean Air Chang-Gong 91 | |||||||||||||||
| 释义 |
The Korean Air Chang-Gong 91 ({{lang-en|Blue Sky 91}}) is a four-seat single-engined low-wing monoplane designed by the Korea Institute of Aeronautical Technology[1] and built by the Aerospace Division of Korean Air.[2] Specifications{{aerospecs|ref=[2] |met or eng?=met |crew=1 |capacity=3 |length m=7.74 |length ft=25 |length in=5 |span m=10.2 |span ft=33 |span in=5 |swept m= |swept ft= |swept in= |rot number= |rot dia m= |rot dia ft= |rot dia in= |dia m= |dia ft= |dia in= |width m= |width ft= |width in= |height m=2.7 |height ft=8 |height in=10 |wing area sqm=14.86 |wing area sqft=160 |swept area sqm= |swept area sqft= |rot area sqm= |rot area sqft= |volume m3= |volume ft3= |aspect ratio= |empty weight kg=839 |empty weight lb=1850 |gross weight kg=1225 |gross weight lb=2700 |lift kg= |lift lb= |eng1 number=1 |eng1 type=Lycoming IO-360-A1B6 piston engine |eng1 kw=149 |eng1 hp=200 |eng1 kn= |eng1 lbf= |eng1 kn-ab= |eng1 lbf-ab= |eng2 number= |eng2 type= |eng2 kw= |eng2 hp= |eng2 kn= |eng2 lbf= |eng2 kn-ab= |eng2 lbf-ab= |max speed kmh=339 |max speed mph=210 |max speed mach= |cruise speed kmh= |cruise speed mph= |range km=1500 |range miles=932 |endurance h= |endurance min= |ceiling m=5025 |ceiling ft=16,500 |glide ratio= |climb rate ms= |climb rate ftmin= |sink rate ms= |sink rate ftmin= |armament1= |armament2= |armament3= |armament4= |armament5= |armament6= }} See also{{aircontent|see also= |related= |similar aircraft=
|sequence= |lists= }} ReferencesNotes1. ^{{cite journal | title= Korean industry makes show debut | journal= Flight International | page= 13| date= 1989-08-26}} 2. ^1 Taylor 1996, p.408 Bibliography{{refbegin}}
1 : Aircraft manufactured in South Korea |
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