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Text File  |  1994-06-27  |  509b  |  31 lines
  1. wing_lift_coeff 7
  2. wing_incidence 145
  3. wing_dihedral 0
  4. adverse_yaw 3
  5. stall_angle 3640
  6. ac_max_thrust 1024
  7. ac_max_speed 6170
  8. ac_stall_speed 1050
  9. real_weight 30000
  10. standard_weight 1024
  11. start_fuel 136
  12. elevator_max 6370
  13. rudder_max 3640
  14. pitch_control 10
  15. roll_control 9
  16. yaw_control 9
  17. pitch_stability 62
  18. yaw_stability 59
  19. pitch_inertia 35
  20. roll_inertia 31
  21. yaw_inertia 36
  22. pitch_drag 15
  23. roll_drag 10
  24. yaw_drag 17
  25. x_drag 45
  26. y_drag 135
  27. clean_drag 11
  28. air_brake_drag 11
  29. gear_drag 8
  30. engine_drag 173
  31.