; AeroTech L1150
; provided by ThrustCurve.org (www.thrustcurve.org)
L1150 75 531 0 2.06528 3.6736 AT
   0.053 935.855
   0.175 1292.642
   0.300 1260.926
   0.425 1241.482
   0.550 1257.058
   0.675 1272.287
   0.800 1287.605
   0.925 1301.012
   1.048 1309.708
   1.170 1308.417
   1.295 1304.830
   1.420 1285.265
   1.545 1267.657
   1.670 1255.624
   1.795 1227.212
   1.920 1202.443
   2.043 1182.617
   2.165 1150.712
   2.290 1117.909
   2.415 1081.739
   2.540 1037.547
   2.665 1007.091
   2.790 1008.911
   2.915 643.124
   3.040 64.371
   3.165 0.000
;