| 词条 | Holmes KH-1 | |||||||||||||||||
| 释义 |
The Holmes KH-1 is a British single-seat high-performance homebuilt sailplane designed and built by Kenneth Holmes and first flown on 27 November 1971. DesignThe KH-1 is a shoulder-wing cantilever monoplane with a conventional all-wood semi-monocoque fuselage and tail unit with an all-moving tailplane, the wings have small-span flaps for control during approach but no airbrakes or spoilers. The pilot has a semi-reclined seat in an enclosed cockpit under a two-piece transparent canopy. The KH-1 landing gear is a retractable monowheel gear and a tailskid, it is also fitted with a tail drag chute to control speed during approach. Specifications{{aerospecs|ref=Jane's All the World's Aircraft 1973-74 |met or eng?=met |genhide= |crew=1 |capacity= |length m=7.315 |length ft=24 |length in=0 |span m=18.56 |span ft=61 |span in=0 |height m= |height ft= |height in= |wing area sqm=11.70 |wing area sqft=126 |aspect ratio= |empty weight kg=226 |empty weight lb=500 |gross weight kg=325 |gross weight lb=716 |eng1 number= |eng1 type= |eng2 number= |eng2 type= |perfhide= |max speed kmh=158 |max speed mph=97.5 |stall speed kmh=67 |stall speed mph=41.5 |range km= |range miles= |endurance h= |endurance min= |ceiling m= |ceiling ft= |glide ratio= |sink rate ms= |sink rate ftmin= }}{{aircontent |see also= |related= |similar aircraft= |lists= }} ReferencesNotesBibliography{{refbegin}}
External links
3 : British sailplanes 1970–1979|Homebuilt aircraft|Glider aircraft |
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