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DATA
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WILDNOV.FMD
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1994-11-12
|
555b
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45 lines
FST_Model 1
airframe_weight 7876
airframe_drag 1.50
uc_drag 3.50
airbrake_drag 1.00
dihedral 3.50
incidence 1.00
stall_angle 18.00
wing_efficiency 0.45
control_power 1.40
roll_inertia 4.00
pitch_inertia 5.00
retracts 1
flaps 1
airbrakes 0
biplane 0
tail_dragger 1
ejector 1
thrust 2150
fuel_weight 1451
num_engines 1
jet_engine 0
units_per_meter 10
grid_space 10
x_centre 204
39 0
18 8
-13 8
18 -8
-13 -8
-36 0
-54 0
14 57
-11 56
14 -57
-11 -56
-43 23
-53 22
-43 -23
-53 -22
-126 171
-141 176
-113 200
-141 200