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DATA
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P-26.FMD
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Text File
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1994-10-18
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552b
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45 lines
FST_Model 1
airframe_weight 3012
airframe_drag 1.70
uc_drag 0.20
airbrake_drag 1.00
dihedral 2.00
incidence 1.00
stall_angle 18.00
wing_efficiency 1.00
control_power 0.70
roll_inertia 4.00
pitch_inertia 5.00
retracts 0
flaps 1
airbrakes 0
biplane 0
tail_dragger 1
ejector 1
thrust 2160
fuel_weight 800
num_engines 1
jet_engine 0
units_per_meter 10
grid_space 10
x_centre 204
30 0
15 8
-10 7
15 -8
-10 -7
-36 0
-51 0
10 46
-4 46
10 -46
-4 -46
-42 15
-50 18
-42 -15
-50 -18
-127 179
-139 181
-117 200
-139 200