Agusta-Bell AB.102
From Wikipedia, the free encyclopedia
AB.102 | |
---|---|
Type | Utility helicopter |
Manufacturer | Agusta |
Maiden flight | 1959 |
Primary user | Elivie |
The Agusta AB.102 was an Italian helicopter produced in small numbers in the early 1960s. The aircraft was based on the mechanical components of a Bell 48 that Agusta incorporated into an all-new, streamlined fuselage. The first flight was on 3 February 1959 and the prototype was exhibited at that year's Paris Air Show in faux military colours.
Two examples were operated by Elivie in a regular air service between Turin and Milan from 1961. However, the advent of turbine-powered helicopters in the 1960s soon rendered the AB.102 obsolete.
[edit] Specifications
General characteristics
- Crew: 1-2 pilots
- Capacity: 7-9 passengers or 880 kg (1,940 lb) cargo or 4 stretchers and 1 attendant
- Length: 17.92 m (58 ft 10 in)
- Main rotor diameter: 14.5 m (47 ft 6 in)
- Height: 3.23 m (10 ft 7 in)
- Main rotor area: 165 m² (1,780 ft²)
- Empty weight: 1,810 kg (3,990 lb)
- Gross weight: 3,025 kg (6,670 lb)
- Powerplant: 1 × Pratt & Whitney R-1340-S1H4 radial, 447 kW (600 hp)
Performance
- Maximum speed: 177 km/h (110 mph)
- Range: 400 km (250 miles)
- Service ceiling: 3,900 m (12,800 ft)
[edit] References
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions, 40.
- Simpson, R. W. (1998). Airlife's Helicopters and Rotorcraft. Ramsbury: Airlife Publishing, 36.
[edit] Related content
Designation sequence
A.101 - AB.102 - A.103 - A.104 - A.105
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