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F-15 stol/mtd aoa research vehicle 4

618 Myplanes  6.1 years ago
33 downloads
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Thrust vectoring in the pitch, yaw, and roll axes. Canards for roll control at high angles of attack.

General Characteristics

Performance

  • Power/Weight Ratio 4.063
  • Wing Loading 16.6lbs/ft2 (81.2kg/m2)
  • Wing Area 998.1ft2 (92.7m2)
  • Drag Points 4420

Parts

  • Number of Parts 59
  • Control Surfaces 6
  • Performance Cost 513