--- /dev/null
+; Entered by Tim Van Milligan. Used John Coker's ThrustCurve Tracer software and\r
+; data supplied by Aerotech thrust stand data. The total weight is a guess.\r
+L339N 98 309 4 1.796 4.5 Aerotech\r
+ 0.049 2.884\r
+ 0.074 373.449\r
+ 0.123 399.403\r
+ 0.156 408.054\r
+ 0.279 415.984\r
+ 0.427 417.426\r
+ 0.476 421.031\r
+ 0.509 416.705\r
+ 0.632 415.984\r
+ 0.837 414.542\r
+ 0.894 418.868\r
+ 0.943 405.17\r
+ 1.026 400.124\r
+ 1.124 402.286\r
+ 1.255 397.961\r
+ 1.362 392.914\r
+ 1.51 391.472\r
+ 1.575 394.356\r
+ 1.592 385.705\r
+ 1.657 387.147\r
+ 1.838 384.984\r
+ 2.026 382.821\r
+ 2.174 379.937\r
+ 2.404 377.053\r
+ 2.478 378.495\r
+ 2.552 377.053\r
+ 2.617 378.495\r
+ 2.683 366.96\r
+ 2.773 359.751\r
+ 2.806 363.355\r
+ 2.937 359.751\r
+ 3.232 351.099\r
+ 3.314 355.425\r
+ 3.356 351.099\r
+ 3.815 345.332\r
+ 3.979 340.285\r
+ 4.233 336.681\r
+ 4.414 333.797\r
+ 4.668 330.913\r
+ 4.996 329.471\r
+ 5.39 323.704\r
+ 5.686 320.099\r
+ 5.989 314.331\r
+ 6.178 310.727\r
+ 6.325 306.401\r
+ 6.514 302.075\r
+ 6.621 302.075\r
+ 6.851 297.75\r
+ 7.195 290.54\r
+ 7.277 293.424\r
+ 7.326 287.656\r
+ 7.441 283.331\r
+ 7.49 286.214\r
+ 7.54 283.331\r
+ 7.696 275.4\r
+ 7.81 273.958\r
+ 7.884 276.842\r
+ 7.942 278.284\r
+ 8.015 276.121\r
+ 8.073 270.354\r
+ 8.188 155.003\r
+ 8.212 118.956\r
+ 8.278 54.071\r
+ 8.311 26.675\r
+ 8.352 7.93\r
+ 8.426 0.0\r