| 词条 | Borel Bo.11 | |||||||||||||||
| 释义 |
The Borel Bo.11 was a French two-seat general purpose monoplane designed and built by Etablissements Borel. Design and developmentThe Bo.11 was mid-wing monoplane from 1911 with wire-braced wings and lateral control by wing warping. It was powered by a {{convert|70|hp|kW|abbr=on|order=flip}} Gnome rotary piston engine. The Bo.11 served with the Aéronautique Militaire at military air training schools and at a civil flying school at Buc. The aircraft could be fitted with twin floats. Specifications{{aerospecs|ref=The Illustrated Encyclopedia of Aircraft |met or eng?=met |genhide= |crew=2 |capacity= |length m=6.70 |length ft=21 |length in=11¾ |span m=9.60 |span ft=31 |span in=6 |height m=2.50 |height ft=8 |height in=2½ |wing area sqm= |wing area sqft= |empty weight kg= |empty weight lb= |gross weight kg= |gross weight lb= |eng1 number=1 |eng1 type=Gnome rotary piston engine |eng1 kw=52 |eng1 hp=70 |eng2 number= |eng2 type= |perfhide= |max speed kmh=90 |max speed mph=56 |cruise speed kmh=70 |cruise speed mph=43 |range km= |range miles= |ceiling m= |ceiling ft= |climb rate ms= |climb rate ftmin= }} See also{{aircontent||related= |similar aircraft=
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6 : French military utility aircraft 1910–1919|Floatplanes|Borel aircraft|Single-engined tractor aircraft|Rotary-engined aircraft|Aircraft first flown in 1911 |
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