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Agusta A.103

In October 1959, the Agusta A.103, a single-seat light helicopter, took flight as an Italian prototype.

The pilot enjoyed an enclosed cockpit made of perspex, while the engine was positioned at the rear. Additionally, the tail rotor was mounted on an enclosed boom.

Specifications

Crew

1

Length

6.13 m (20 ft 1 in)

Height

2.23 m (7 ft 4 in)

Empty weight

280 kg (617 lb)

Gross weight

460 kg (1,014 lb)

Powerplant

1 × Agusta GA.70 air-cooled flat-four engine,

63 kW (85 hp)

Main rotor diameter

7.40 m (24 ft 3 in)

Performance

Maximum speed

150 km/h (93 mph, 81 kn)

Cruise speed

135 km/h (84 mph, 73 kn)

Range

450 km (280 mi, 240 nmi)

Endurance

3 hr 20 min

Service ceiling

2,000 m (6,600 ft) (hover ceiling in ground effect)

Rate of climb

4.0 m/s (787 ft/min).

Sources

Airlife’s Helicopters and Rotorcraft-R W Simpson.

Jane’s Encyclopaedia of Aviation-M J H Taylor.

 

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