词条 | Montana Coyote | |||||||||||||||
释义 |
The Montana Coyote is an American single-engined two-seat STOL aircraft designed for home building by Montana Coyote Inc. of Helena, Montana. Design and developmentThe Coyote is a high-wing strut-braced monoplane first flown in early 1991 and sold as kit for home building without an engine. With a steel tube fuselage and wooden wings it is designed to take an engine between 100 and 200 hp (74 to 149 kW) as long as it weighs less than 350 lb (159 kg). It has a fixed tailwheel type landing gear with a cabin for a pilot and passenger side-by-side, it is designed to land and take-off within 350 ft (107 m). Specifications{{aerospecs|ref=Jane's All the World's Aircraft 1995-1996 |met or eng?=eng |genhide= |crew=1 |capacity=1 passenger |length m=7.62 |length ft=25 |length in=0 |span m=11.58 |span ft=38 |span in=0 |height m=1.98 |height ft=6 |height in=6 |wing area sqm=15.40 |wing area sqft=165.75 |empty weight kg=408 to 476 |empty weight lb=900 to 1050 |gross weight kg=839 |gross weight lb=1850 |eng1 number=1 |eng1 type=piston engine |eng1 kw=74 to 149 |eng1 hp=100 to 200 |eng2 number= |eng2 type= |perfhide= |max speed kmh=193 |max speed mph=120 |cruise speed kmh=161 |cruise speed mph=100 |stall speed kmh=57 |stall speed mph=35 |range km=1804 |range miles=500 |ceiling m=4575 |ceiling ft=15000 |climb rate ms=6.4 |climb rate ftmin=1250 }}{{aircontent |see also= |related= |similar aircraft= |lists= }} ReferencesNotesBibliography{{refbegin}}
2 : United States civil utility aircraft 1990–1999|Homebuilt aircraft |
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