Glasair I
From Wikipedia, the free encyclopedia
The Glasair I, originally built as the prototype Glasair TD taildragger, is a high-performance homebuilt aircraft built of fiberglass. Created by Tom Hamilton as a fast, two-seat kitplane, the Glasair TD first flew in 1979. Hamilton formed Stoddard-Hamilton Aircraft that year to produce and market the kit, which was the first pre-molded composite aircraft available to builders.
[edit] Specifications ()
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
- Length: ft in (m)
- Wingspan: ft in (m)
- Height: ft in (m)
- Wing area: ft (m)
- Empty weight: lb (kg)
- Loaded weight: lb (kg)
- Useful load: lb (kg)
- Max takeoff weight: lb (kg)
Performance
- Never exceed speed: mph (km/h)
- Maximum speed: mph (km/h)
- Cruise speed: mph (km/h)
- Stall speed: mph (km/h)
- Range: mi (km)
- Service ceiling: ft (m)
- Rate of climb: ft/min (m/s)
- Wing loading: lb/ft² (kg/m²)
