The Kindacanard is an experimental plane used to test wingplans for high manouverability and stability at high speeds. It combines a shallow delta wing and forward angled tandem wing / extreme canard.
The usual controls, Trim for pitch trim and VTOL for flaps
AG1 for navigation/anti-collision lights and AG2 for cocpit canopy
Specifications
General Characteristics
- Created On Windows
- Wingspan 65.4ft (19.9m)
- Length 44.2ft (13.5m)
- Height 13.4ft (4.1m)
- Empty Weight 17,217lbs (7,809kg)
- Loaded Weight 31,617lbs (14,341kg)
Performance
- Power/Weight Ratio 21.323
- Wing Loading 47.2lbs/ft2 (230.4kg/m2)
- Wing Area 670.1ft2 (62.3m2)
- Drag Points 4693
Parts
- Number of Parts 91
- Control Surfaces 9
- Performance Cost 696
