词条 | Lammer Geyer Jupiter | |||||||||||||||||
释义 |
The Lammer Geyer Jupiter is a South African four-seat cabin monoplane designed by Lammer Geyer Aviation for sale as a kit for amateur construction. Design and developmentDesign on the Jupiter started in 1996 and the prototype, registered ZU-CNH first flew on 1 December 2002. The Jupiter is an all-composite low-wing cantilever monoplane with a fixed tricycle landing gear. The prototype is powered by a {{convert|210|hp|kW|0|abbr=on}} Continental IO-360 flat-six engine with a three-bladed tractor propeller. The cabin has room for four seated side-by-side in two rows. Specifications (prototype){{aerospecs|ref=Jane's All the World's Aircraft 1989-90 |met or eng?=met |genhide= |crew=one |capacity=three |length m=7.25 |length ft=23 |length in=9½ |span m=9.80 |span ft=32 |span in=1¾ |height m=2.36 |height ft=7 |height in=9 |wing area sqm=15.50 |wing area sqft=166.8 |aspect ratio=6.2 |empty weight kg=560 |empty weight lb=1235 |gross weight kg=1025 |gross weight lb=2259 |eng1 number=1 |eng1 type=Continental IO-360 flat-six |eng1 kw=157 |eng1 hp=210 |eng2 number= |eng2 type= |perfhide= |max speed kmh=281 |max speed mph=175 |cruise speed kmh=253 |cruise speed mph=157 |stall speed kmh=80 |stall speed mph=50 |range km=2000 |range miles=1242 |ceiling m=8230 |ceiling ft=27000 |g limits=+6/-3.5 |climb rate ms= |climb rate ftmin=1970 }}{{aircontent |see also= |related= |similar aircraft= |lists= }} ReferencesNotesBibliography{{refbegin}}
6 : South African civil utility aircraft 2000-2009|Homebuilt aircraft|Single-engined tractor aircraft|Low-wing aircraft|Lammer Geyer aircraft|Aircraft first flown in 2002 |
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