| 词条 | Comte AC-8 | |||||||||||||||
| 释义 |
The Comte AC-8 was a 1930s Swiss six-seat light transport aircraft produced by Flugzeugbau A. Comte. Design and developmentSimilar in configuration to the company's earlier Comte AC-4, the Comte AC-8 was designed as a light transport for five passengers. It incorporated a braced high-wing monoplane wing, with a conventional tail unit and fixed tailwheel landing gear. The enclosed cabin had accommodation for a pilot and five passengers. The aircraft was powered by either a Wright J-6 or Lorraine radial engine. Only three aircraft were built. Specifications{{aerospecs|ref= |met or eng?=met |crew=1 |capacity=5 |length m=9.2 |length ft=30 |length in=2¼ |span m=14.5 |span ft=47 |span in=6¾ |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=2.9 |height ft=9 |height in=6 |wing area sqm=28 |wing area sqft=301.4 |swept area sqm= |swept area sqft= |rot area sqm= |rot area sqft= |volume m3= |volume ft3= |aspect ratio= |empty weight kg=1115 |empty weight lb=2,458 |gross weight kg=1750 |gross weight lb=3,858 |lift kg= |lift lb= |eng1 number=1 |eng1 type=Wright J-6 radial piston engine |eng1 kw=224 |eng1 hp=300 |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=214 |max speed mph=133 |max speed mach= |cruise speed kmh= |cruise speed mph= |range km=900 |range miles=559 |endurance h= |endurance min= |ceiling m=5000 |ceiling ft=16,405 |glide ratio= |climb rate ms= |climb rate ftmin= |sink rate ms= |sink rate ftmin= |armament1= |armament2= |armament3= |armament4= |armament5= |armament6= }} References{{commons category|Comte aircraft}}
See also{{aircontent|related= |similar aircraft= |lists= |see also= }}{{Comte aircraft}} 3 : Swiss civil utility aircraft 1930–1939|Comte aircraft|Single-engined tractor aircraft |
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