Engineering:American Air Jet American
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Revision as of 13:00, 19 June 2022 by imported>Jslovo (fix)
| American | |
|---|---|
| Role | Homebuilt helicopter |
| National origin | United States |
| Manufacturer | American Air Jet |
| First flight | 1988 |
The American Air Jet American is an American homebuilt tip jet helicopter designed and built by American Air Jet of Woodland Park, Colorado for amateur construction from kits.[1]
Design and development
The American is either a tandem two-seat or single seat helicopter first flown in July 1988. It has an aluminium alloy enclosed cockpit with a twin skid landing gear and non-moving tail surfaces. The American has a twin-blade single rotor made from glassfibre and no tail rotor, on the prototype a 280 hp (209 kW) Wankel rotary engine drives a centrifugal compressor that provides air to thrust jets on the tips of the blades.[1]
Specifications (Prototype)
Data from Jane's All the World's Aircraft 1989-90[1]
General characteristics
- Crew: 1
- Length: 18 ft 0 in (5.49 m)
- Height: 8 ft 0 in (2.44 m)
- Empty weight: 980 lb (445 kg)
- Gross weight: 1,600 lb (726 kg)
- Powerplant: 1 × Wankel rotary engine , 208 hp (109 kW)
- Main rotor diameter: 36 ft 0 in (10.97 m)
Performance
- Maximum speed: 90 mph (145 km/h, 78 kn)
- Cruise speed: 70 mph (113 km/h, 61 kn)
- Range: 300 mi (483 km, 260 nmi)
- Service ceiling: 10,000 ft (3,050 m)
See also
Related lists
References
Notes
Bibliography
- Taylor, John W.R., ed (1989). Jane's All the World's Aircraft 1989-90. London, United Kingdom: Jane's Yearbooks. ISBN 0-7106-0896-9.
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