| 词条 | Agusta A.104 | |||||||||||||||
| 释义 |
The Agusta A.104 Helicar was an Italian prototype light commercial helicopter first flown in December 1960. ProductionThe A.104 was a slightly enlarged version of the A.103, and added a second seat beside the pilot's seat. The cockpit was enclosed by a perspex bubble with the engine at the rear and the tail rotor carried on an enclosed boom. Two piston-engined prototypes were built, followed by a single example of a turbine-engined variant designated A.104BT. No production resulted. Surviving aircraftAn example of the A.104 is preserved in the Museo Agusta which is maintained by the Agusta company and is located just south of Milan Malpensa Airport[1] Variants
Specifications{{aerospecs|met or eng?=met |ref=Jane's All The World's Aircraft 1961–62[2] |crew=one, pilot |capacity=1 passenger |length m=6.35 |length ft=20 |length in=10 |span m= |span ft= |span in= |rot number=1 |rot dia m=7.95 |rot dia ft=26 |rot dia in=1 |height m=2.35 |height ft=7 |height in=7¾ |wing area sqm= |wing area sqft= |rot area sqm=49.6 |rot area sqft=534 |aspect ratio= |empty weight kg=380 |empty weight lb=838 |gross weight kg=640 |gross weight lb=1,400 |eng1 number=1 |eng1 type=Agusta GA.140 (derated) |eng1 kw=104 |eng1 hp=140 |max speed kmh=165 |max speed mph=103 |cruise speed=kmh=135 |cruise speed mph=84 |range km=330 |range miles=205 |endurance h=2 |endurance min=30 |ceiling m=3,000 |ceiling ft=9,840 |climb rate ms=4.1 |climb rate ftmin=810 |sink rate ms= |sink rate ftmin= |armament1= |armament2= |armament3= |armament4= |armament5= |armament6= }} See also{{aircontent|related= |similar aircraft= |lists= |see also= }} References1. ^Ogden, 2006, p. 306 2. ^Taylor 1961, p. 97.
External links{{commons category|Agusta}}
4 : Italian civil utility aircraft 1960–1969|Italian helicopters 1960–1969|Agusta aircraft|Aircraft first flown in 1960 |
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