DESIGN VARIABLES IN CRAGER

• Configuration related

  • Wing Aspect Ratio
  • Wing Area
  • Wing Taper Ratio
  • Wing Thickness Ratio
  • Wing L.E. Location
  • Rear Fuselage Length
  • Take-off Flap Deflection
  • Max. Take-Off mass
  • Total Fuel mass
  • Max. Take-off Power
  • Balanced Field Length

• Trajectory related

  • Climb Throttle
  • Descent Throttle (Initial)
  • Descent Throttle (Final)
  • Climb Speed
  • Cruise Mach Number
  • Descent Speed
  • Cruising Altitude
  • Cruise Fraction (main stage)
  • Cruise Fraction (notional stage)

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