Agusta A.103 Rotorcraft

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Manufacturer
Agusta
Description
The Agusta A.103 was an Italian prototype single-seat light helicopter flown in October 1959.
First Flight
1959-10-01
Designer
Agusta
Type
Light helicopter
Length (m)
6.13
Height (m)
2.23
Cockpit Crew
1
Max Speed (km/h)
150
Cruise Speed (km/h)
135
Max Ceiling (m)
2000
Rate of Climb (m/s)
4
Endurance (h)
3
Powerplant Description
1 × Agusta GA.70 air-cooled flat-four engine, 63 kW (85 hp) each
Wikipedia Article (URL)
en.wikipedia.org/wiki/Agusta_A.103
Aircraft Engine
Agusta GA.70
Number of Engines
1
Number of main rotor blades
1
47 empty fields

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