Advanced Aviation Cobra
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| Cobra | |
|---|---|
| Type | Homebuilt ultralight aircraft |
| Manufacturer | Advanced Aviation |
| Maiden flight | 1980s |
| Primary user | Individual civilians |
The Advanced Aviation Cobra was a U.S. ultralight aircraft of extremely minimalist design marketed for homebuilding. The pilot is seated in an open framework suspended beneath a fabric-covered wing on which the engine (adapted from a snowmobile) and pusher propeller are also mounted. Early Cobras (Model A) had spoliers for roll control, while the Model B had traditional full three-axis control using ailerons. A two-seat training version, known as the King Cobra was also available.
[edit] Specifications (Model B)
This aircraft article is missing some (or all) of its specifications. If you have a source, you can help Wikipedia by adding them.General characteristics
- Crew: 1
- Length: ft in (m)
- Wingspan: 35 ft 0 in (10.7 m)
- Height: ft in (m)
- Wing area: 162 ft² (15 m²)
- Empty weight: 218 lb (99 kg)
- Max takeoff weight: 468 lb (212 kg)
- Powerplant: 1× 430 Cuyuna, 52 hp (39 kW)
Performance
- Maximum speed: 75 mph (65 knots, 120 km/h)
- Range: mi (nm, km)
- Service ceiling: ft (m)
- Rate of climb: ft/min (m/s)
[edit] Related content
Related lists
- List of ultralight aircraft
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