; AeroTech K1100T
; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)
; provided by ThrustCurve.org (www.thrustcurve.org)
K1100T 54 398 0 0.7616 1.32518 AT
   0.034 1234.653
   0.105 1233.429
   0.176 1192.393
   0.247 1163.041
   0.318 1147.963
   0.389 1146.319
   0.460 1140.958
   0.532 1132.640
   0.603 1123.824
   0.674 1108.921
   0.745 1090.974
   0.816 1073.937
   0.887 1049.133
   0.959 1021.216
   1.030 994.559
   1.101 966.571
   1.172 940.194
   1.243 909.792
   1.315 880.264
   1.386 844.477
   1.457 643.599
   1.528 401.861
   1.599 145.498
   1.670 28.372
   1.742 -0.884
   1.814 0.000
;