--- /dev/null
+; AeroTech I218R\r
+; provided by ThrustCurve.org (www.thrustcurve.org)\r
+I218R 38 191 0 0.19264 0.37184 AT\r
+ 0.027 136.078\r
+ 0.088 275.030\r
+ 0.148 280.998\r
+ 0.208 284.371\r
+ 0.268 284.037\r
+ 0.327 279.311\r
+ 0.388 277.791\r
+ 0.448 276.309\r
+ 0.509 269.384\r
+ 0.570 266.041\r
+ 0.630 261.907\r
+ 0.690 256.366\r
+ 0.750 250.565\r
+ 0.810 242.206\r
+ 0.870 234.607\r
+ 0.930 225.488\r
+ 0.991 216.166\r
+ 1.053 205.415\r
+ 1.112 193.238\r
+ 1.173 177.206\r
+ 1.233 161.304\r
+ 1.292 139.118\r
+ 1.353 96.082\r
+ 1.413 38.848\r
+ 1.474 5.978\r
+ 1.535 0.000\r