• Source: Agusta A.103

      • The Agusta A.103 was an Italian prototype single-seat light helicopter flown in October 1959. The pilot was enclosed by a perspex bubble with the engine at the rear and the tail rotor carried on an enclosed boom.


      Specifications


      Data from Jane's All The World's Aircraft 1961–62 General characteristics
      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)


      See also



      Related lists

      List of rotorcraft


      References



      Taylor, John W. R. (1961). Jane's All The World's Aircraft 1961–62. London: Sampson Low, Marston & Company.
      Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 40.
      Simpson, R. W. (1998). Airlife's Helicopters and Rotorcraft. Ramsbury: Airlife Publishing. p. 36.


      External links



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