Post-stall / flat spin recovery research demonstrator
618 Myplanes
6.3 years ago
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Auto Credit Based on weebabyseamus's F-18 Hornet
The canards adjust to aoa in the pitch axis to allow post stall roll control as in the f-15 actvive
Specifications
General Characteristics
- Predecessor F-18 Hornet
- Successors 3 airplane(s)
- Created On iOS
- Wingspan 32.5ft (9.9m)
- Length 42.7ft (13.0m)
- Height 13.1ft (4.0m)
- Empty Weight 7,618lbs (3,455kg)
- Loaded Weight 11,264lbs (5,109kg)
Performance
- Power/Weight Ratio 2.992
- Wing Loading 22.7lbs/ft2 (111.1kg/m2)
- Wing Area 495.1ft2 (46.0m2)
- Drag Points 1954
Parts
- Number of Parts 37
- Control Surfaces 5
- Performance Cost 290
it lacks power recover it's speed