| 词条 | Brochet MB.110 | |||||||||||||||
| 释义 |
The Brochet MB.110 was a four-seat light aircraft developed in France in the early 1950s. Design and developmentA further derivative of the Brochet MB.70 family, generally similar to those aircraft, the MB.110 was a substantially new and enlarged design. Apart from a bigger passenger cabin with one more seat than previous models, the wing and tail were redesigned, and a more powerful engine was fitted. Two examples were built. Specifications{{aerospecs|met or eng?=met |crew=One pilot |capacity=3 passengers |length m=7.68 |length ft=25 |length in=2 |span m=11.06 |span ft=36 |span in=3 |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=2.56 |height ft=8 |height in=5 |wing area sqm=15.7 |wing area sqft=169 |swept area sqm= |swept area sqft= |rot area sqm= |rot area sqft= |volume m3= |volume ft3= |aspect ratio= |empty weight kg=800 |empty weight lb=1,764 |gross weight kg=1,300 |gross weight lb=2,866 |lift kg= |lift lb= |eng1 number=1 |eng1 type=SNECMA-built Regnier 4L |eng1 kw=127 |eng1 hp=170 |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=240 |max speed mph=150 |max speed mach= |cruise speed kmh= |cruise speed mph= |range km=1,000 |range miles=620 |endurance h= |endurance min= |ceiling m= |ceiling ft= |glide ratio= |climb rate ms= |climb rate ftmin= |sink rate ms= |sink rate ftmin= |armament1= |armament2= |armament3= |armament4= |armament5= |armament6= }} References{{commons category|Brochet MB.110}}
|related= |similar aircraft= |lists= |see also= }}{{Brochet aircraft}} 5 : French sport aircraft 1950–1959|Brochet aircraft|High-wing aircraft|Single-engined tractor aircraft|Aircraft first flown in 1956 |
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