; AeroTech K1275R
; provided by ThrustCurve.org (www.thrustcurve.org)
K1275R 54 569 0 1.29024 2.03392 AT
   0.039 1282.616
   0.119 1557.989
   0.199 1540.196
   0.279 1526.782
   0.359 1500.693
   0.440 1456.584
   0.520 1425.794
   0.600 1390.416
   0.680 1355.109
   0.761 1323.311
   0.841 1282.825
   0.921 1247.795
   1.001 1194.417
   1.081 1150.977
   1.162 1108.223
   1.242 1068.754
   1.322 1036.922
   1.403 997.444
   1.482 964.569
   1.563 933.305
   1.644 889.992
   1.724 599.467
   1.804 134.559
   1.884 5.630
   1.964 0.205
   2.045 0.000
;