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/ Agusta A.115
Agusta A.115
The Agusta A.115, which took flight in Italy in 1961, was a prototype helicopter.
It featured a bare, tubular tail boom and was equipped with a Turbomeca Astazou II turboshaft engine.
However, despite its promising design, no further production of this helicopter took place.
Specifications
Crew
1
Capacity
3 passengers
Or
3 stretchers & a medical attendant.
Length
9.91 m (32 ft 6 in)
Height
2.94 m (9 ft 8 in)
Empty weight
730 kg (1,609 lb)
Gross weight
1,350 kg (2,976 lb)
Powerplant
1 × Turbomeca Astazou II turboshaft,
360 kW (480 hp)
Main rotor diameter
11.33 m (37 ft 2 in)
Main rotor area
101 m
2
(1,090 sq ft)
Performance
Maximum speed
170 km/h (110 mph, 92 kn)
Cruise speed
150 km/h (93 mph, 81 kn)
Range
260 km (160 mi, 140 nmi)
Service ceiling
4,750 m (15,580 ft).
Sources
Airlife’s Helicopters and Rotorcraft-R W Simpson.
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