AISA GN
| GN | |
|---|---|
| Role | Autogyro |
| Manufacturer | AISA |
| First flight | 1982 |
| Number built | 1 |
The AISA GN was a prototype four-seat autogyro developed in Spain between 1971 and 1982. it featured an extensively-glazed cabin fitted with a pusher engine and tricycle undercarriage. A separate tail fin was carried at the end of two booms mounted to stub wings. The prototype was developed with a 200 hp engine.[1] The aircraft suffered from an extremely prolonged development, but finally took to the air on 20 July 1982. Shortly thereafter, however, it was damaged and finally abandoned.
Specifications
General characteristics
- Crew: one pilot
- Capacity: 3 passengers
Performance
References
- ^ "none". Air Progress: 19. December 1971.
Wikimedia Commons has media related to AISA aircraft.
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 51.
- Simpson, R. W. (1998). Airlife's Helicopters and Rotorcraft. Ramsbury: Airlife Publishing. p. 207.
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