FST_Model 1
airframe_weight 16000
airframe_drag 1.50
uc_drag 3.50
airbrake_drag 2.00
dihedral 0.00
incidence 0.80
stall_angle 25.00
wing_efficiency 1.00
control_power 1.70
roll_inertia 0.60
pitch_inertia 0.80
retracts 1
flaps 1
airbrakes 1
biplane 0
tail_dragger 0
ejector 1
thrust 14000
fuel_weight 2400
num_engines 1
jet_engine 1
units_per_meter 15
grid_space 15
x_centre 199
88 0
31 14
-45 13
31 -14
-45 -13
-78 0
-120 0
-15 74
-45 74
-15 -74
-45 -74
-106 37
-123 37
-106 -37
-123 -37
-130 156
-150 156
-87 200
-140 200
