X-Git-Url: https://git.gag.com/?a=blobdiff_plain;f=datafiles%2Fthrustcurves%2FAeroTech_L2200.eng;fp=datafiles%2Fthrustcurves%2FAeroTech_L2200.eng;h=e531570cf46830daad79ce012cb5d393556c5184;hb=bf76931b27b597f7bc1dd5a0e7e2460ac065415b;hp=0000000000000000000000000000000000000000;hpb=def27b03bd9ebe6628421ec61112ebe4f45f043d;p=debian%2Fopenrocket

diff --git a/datafiles/thrustcurves/AeroTech_L2200.eng b/datafiles/thrustcurves/AeroTech_L2200.eng
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+++ b/datafiles/thrustcurves/AeroTech_L2200.eng
@@ -0,0 +1,39 @@
+; Curvefit of Aerotech Instructions by C. Kobel  11/19/08
+L2200G 75 665 0-6-10-14-18 2.516 4.751 AT
+   0.011 1195.177
+   0.024 2029.903
+   0.037 2380.868
+   0.050 2542.122
+   0.100 2570.578
+   0.150 2561.093
+   0.200 2523.151
+   0.250 2485.208
+   0.300 2523.151
+   0.350 2570.578
+   0.400 2674.919
+   0.500 2912.057
+   0.600 3073.311
+   0.700 3073.311
+   0.800 3101.768
+   0.900 3092.282
+   1.000 3092.282
+   1.100 2959.485
+   1.186 2807.716
+   1.227 2437.781
+   1.270 2257.556
+   1.300 2162.701
+   1.400 1991.961
+   1.500 1878.135
+   1.600 1792.765
+   1.700 1688.424
+   1.800 1612.54
+   1.900 1584.083
+   2.000 1536.656
+   2.048 1498.714
+   2.084 1403.858
+   2.102 1166.72
+   2.134 796.784
+   2.186 455.305
+   2.237 237.138
+   2.300 94.855
+   2.400 0.0