| 词条 | Boisavia Anjou | |||||||||||||||
| 释义 |
The Boisavia B.260 Anjou (later developed by SIPA as the Sipavia Anjou) was a four-seat twin-engine light aircraft developed in France in the 1950s. It was a low-wing cantilever monoplane of conventional configuration with retractable tricycle undercarriage. Intended by Boisavia as a touring aircraft, it did not find a market and only the single prototype was constructed. At this point, the firm sold the design to SIPA, which modified the design and re-engined it with Lycoming O-360 engines, but found that they could not sell it either. At a time when the twin-engine light plane market was already dominated by all-metal American aircraft, the Anjou's fabric-over-tube construction was something of an anachronism, and all development was soon ceased. Plans to develop a stretched version with three extra seats and Potez 4D engines were also abandoned. Variants
Specifications (B.260){{aerospecs|met or eng?=met |crew=one pilot |capacity=3 passengers |length m=7.10 |length ft=23 |length in=3 |span m=12.85 |span ft=42 |span in=2 |height m= |height ft= |height in= |wing area sqm=21.5 |wing area sqft=231 |aspect ratio= |empty weight kg=992 |empty weight lb=2,187 |gross weight kg=1,870 |gross weight lb=4,123 |eng1 number=2 |eng1 type=SNECMA licence-built Regnier 4L-02 |eng1 kw=127 |eng1 hp=170 |max speed kmh=260 |max speed mph=160 |cruise speed kmh= |cruise speed mph= |range km=1,250 |range miles=780 |endurance h= |endurance min= |ceiling m=7,125 |ceiling ft=23,370 |glide ratio= |climb rate ms=6.0 |climb rate ftmin=1,180 |armament1= |armament2= |armament3= |armament4= |armament5= |armament6= }} References{{commons category|Boisavia}}
7 : Boisavia aircraft|Abandoned civil aircraft projects|French civil utility aircraft 1950–1959|SIPA aircraft|Twin-engined tractor aircraft|Low-wing aircraft|Aircraft first flown in 1956 |
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