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DATA
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DAUNTLS.FMD
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1995-01-22
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556b
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45 lines
FST_Model 1
airframe_weight 6345
airframe_drag 1.80
uc_drag 1.50
airbrake_drag 10.00
dihedral 5.00
incidence 1.00
stall_angle 18.00
wing_efficiency 1.00
control_power 1.10
roll_inertia 6.00
pitch_inertia 7.00
retracts 1
flaps 1
airbrakes 1
biplane 0
tail_dragger 1
ejector 1
thrust 3600
fuel_weight 2000
num_engines 1
jet_engine 0
units_per_meter 10
grid_space 10
x_centre 204
17 0
1 10
-36 8
1 -10
-36 -8
-66 0
-86 0
-6 71
-29 71
-6 -71
-29 -71
-74 30
-83 32
-74 -30
-83 -32
-138 172
-157 172
-126 200
-162 200