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Post-stall / flat spin recovery research demonstrator

618 Myplanes  6.2 years ago
227 downloads
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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

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