X-Git-Url: https://git.gag.com/?a=blobdiff_plain;f=datafiles%2Fthrustcurves%2FAeroTech_I200.eng;fp=datafiles%2Fthrustcurves%2FAeroTech_I200.eng;h=bd7545fc8caf6d791081c2f2ecc6c009ea5091e1;hb=720d4935bc6bec453e6478ad5227356c626610a2;hp=0000000000000000000000000000000000000000;hpb=4bf5c4a7c42d9d494a088be85bcf6bb38ec6d86b;p=debian%2Fopenrocket

diff --git a/datafiles/thrustcurves/AeroTech_I200.eng b/datafiles/thrustcurves/AeroTech_I200.eng
new file mode 100644
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--- /dev/null
+++ b/datafiles/thrustcurves/AeroTech_I200.eng
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+; AeroTech I200W
+; Copyright Tripoli Motor Testing 1999 (www.tripoli.org)
+; provided by ThrustCurve.org (www.thrustcurve.org)
+I200W 29 333 0 0.181888 0.357504 AT
+   0.033 303.951
+   0.103 273.452
+   0.174 276.061
+   0.245 271.625
+   0.316 268.233
+   0.386 258.449
+   0.457 252.480
+   0.528 246.642
+   0.599 242.304
+   0.670 237.737
+   0.741 234.769
+   0.811 233.171
+   0.882 230.660
+   0.953 224.985
+   1.024 221.658
+   1.095 214.548
+   1.166 177.365
+   1.236 154.208
+   1.307 119.146
+   1.378 91.586
+   1.449 65.330
+   1.520 32.877
+   1.591 28.702
+   1.661 22.211
+   1.732 15.558
+   1.803 0.000