| 词条 | Brochet MB.120 | |||||||||||||||
| 释义 |
The Brochet MB.120 was a two-seat light aircraft developed in France in the 1950s. Design and developmentA derivative of the Brochet MB.70 family, combining the wing of the MB.80 with a modified fuselage of the MB.100 seating two. The design never progressed past a single prototype. Specifications{{aerospecs|met or eng?=met |crew=One pilot |capacity=1 passenger |length m=6.50 |length ft=21 |length in=4 |span m=10.65 |span ft=34 |span in=11 |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= |height ft= |height in= |wing area sqm= |wing area sqft= |swept area sqm= |swept area sqft= |rot area sqm= |rot area sqft= |volume m3= |volume ft3= |aspect ratio= |empty weight kg= |empty weight lb= |gross weight kg=765 |gross weight lb=1,687 |lift kg= |lift lb= |eng1 number=1 |eng1 type=Continental C90 |eng1 kw=67 |eng1 hp=90 |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=195 |max speed mph=122 |max speed mach= |cruise speed kmh= |cruise speed mph= |range km= |range miles= |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}}
5 : French sport aircraft 1950–1959|Brochet aircraft|High-wing aircraft|Single-engined tractor aircraft|Aircraft first flown in 1954 |
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