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DATA
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B17.FMD
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Text File
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1994-12-18
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552b
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45 lines
FST_Model 1
airframe_weight 31150
airframe_drag 7.00
uc_drag 2.50
airbrake_drag 4.00
dihedral 5.50
incidence 1.00
stall_angle 18.00
wing_efficiency 1.00
control_power 1.10
roll_inertia 5.00
pitch_inertia 7.00
retracts 1
flaps 1
airbrakes 1
biplane 0
tail_dragger 1
ejector 1
thrust 17280
fuel_weight 25000
num_engines 4
jet_engine 0
units_per_meter 5
grid_space 5
x_centre 204
51 0
27 8
-9 8
27 -8
-9 -8
-38 0
-60 0
19 74
-2 74
19 -74
-2 -74
-49 30
-59 33
-49 -30
-59 -33
-129 158
-145 165
-114 200
-147 200