+; Curvefit of Aerotech Instructions by C. Kobel 11/19/08\r
+L2200G 75 665 0-6-10-14-18 2.516 4.751 AT\r
+ 0.011 1195.177\r
+ 0.024 2029.903\r
+ 0.037 2380.868\r
+ 0.050 2542.122\r
+ 0.100 2570.578\r
+ 0.150 2561.093\r
+ 0.200 2523.151\r
+ 0.250 2485.208\r
+ 0.300 2523.151\r
+ 0.350 2570.578\r
+ 0.400 2674.919\r
+ 0.500 2912.057\r
+ 0.600 3073.311\r
+ 0.700 3073.311\r
+ 0.800 3101.768\r
+ 0.900 3092.282\r
+ 1.000 3092.282\r
+ 1.100 2959.485\r
+ 1.186 2807.716\r
+ 1.227 2437.781\r
+ 1.270 2257.556\r
+ 1.300 2162.701\r
+ 1.400 1991.961\r
+ 1.500 1878.135\r
+ 1.600 1792.765\r
+ 1.700 1688.424\r
+ 1.800 1612.54\r
+ 1.900 1584.083\r
+ 2.000 1536.656\r
+ 2.048 1498.714\r
+ 2.084 1403.858\r
+ 2.102 1166.72\r
+ 2.134 796.784\r
+ 2.186 455.305\r
+ 2.237 237.138\r
+ 2.300 94.855\r
+ 2.400 0.0\r