FST_Model 1
airframe_weight 5000
airframe_drag 2.00
uc_drag 7.00
airbrake_drag 2.00
dihedral 0.02
incidence 2.00
stall_angle 15.00
wing_efficiency 2.00
control_power 4.00
roll_inertia 6.00
pitch_inertia 5.00
retracts 1
flaps 1
airbrakes 1
biplane 0
tail_dragger 0
ejector 1
thrust 6000
fuel_weight 1000
num_engines 2
jet_engine 1
units_per_meter 10
grid_space 20
x_centre 204
88 0
37 14
-30 10
37 -14
-30 -10
-100 0
-140 0
-45 110
-75 110
-45 -110
-75 -110
-135 40
-155 40
-135 -40
-155 -40
-130 150
-150 150
-80 200
-140 200
