X-Git-Url: https://git.gag.com/?a=blobdiff_plain;f=datafiles%2Fthrustcurves%2FAeroTech_F39.eng;fp=datafiles%2Fthrustcurves%2FAeroTech_F39.eng;h=8ea0d81d151c33f8eead8e6210b3372bd401112d;hb=720d4935bc6bec453e6478ad5227356c626610a2;hp=0000000000000000000000000000000000000000;hpb=4bf5c4a7c42d9d494a088be85bcf6bb38ec6d86b;p=debian%2Fopenrocket

diff --git a/datafiles/thrustcurves/AeroTech_F39.eng b/datafiles/thrustcurves/AeroTech_F39.eng
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+; Aerotech F39 RASP.ENG file made from NAR published data
+; File produced July 4, 2000
+; Submitted to ThrustCurve.org by Chris Kobel (4/6/07)
+; The total impulse, peak thrust, average thrust and burn time are
+; the same as the averaged static test data on the NAR web site in
+; the certification file. The curve drawn with these data points is as
+; close to the certification curve as can be with such a limited
+; number of points (32) allowed with wRASP up to v1.6.
+F39T  24   70   3-6-9   .0227   .059   AT
+   0.010   45.057
+   0.016   54.131
+   0.046   58.321
+   0.079   59.470
+   0.103   58.311
+   0.130   57.253
+   0.172   55.491
+   0.235   53.738
+   0.321   51.271
+   0.363   50.566
+   0.387   49.509
+   0.408   50.203
+   0.426   48.804
+   0.453   47.746
+   0.480   47.041
+   0.680   41.059
+   0.716   39.649
+   0.752   38.944
+   0.809   36.487
+   0.860   34.382
+   0.893   33.324
+   0.917   32.619
+   1.000   28.752
+   1.075   25.247
+   1.105   22.095
+   1.126   17.201
+   1.144   13.001
+   1.174    8.109
+   1.219    4.606
+   1.261    2.500
+   1.330    0.000