FST_Model 1
airframe_weight 5000
airframe_drag 2.00
uc_drag 0.50
airbrake_drag 1.00
dihedral 0.00
incidence 2.00
stall_angle 15.00
wing_efficiency 1.50
control_power 2.00
roll_inertia 1.50
pitch_inertia 1.00
retracts 1
flaps 1
airbrakes 1
biplane 0
tail_dragger 0
ejector 1
thrust 3000
fuel_weight 1000
num_engines 1
jet_engine 1
units_per_meter 10
grid_space 20
x_centre 204
96 0
79 40
-40 40
79 -40
-40 -40
-57 0
-81 0
34 201
-29 200
34 -201
-29 -200
-50 41
-67 41
-50 -41
-67 -41
-141 100
-158 100
-60 200
-180 200
