X-Git-Url: https://git.gag.com/?a=blobdiff_plain;f=datafiles%2Fthrustcurves%2FAeroTech_D13.eng;fp=datafiles%2Fthrustcurves%2FAeroTech_D13.eng;h=eec171aa8b675ea876e8ac132e98073c139f1f45;hb=720d4935bc6bec453e6478ad5227356c626610a2;hp=0000000000000000000000000000000000000000;hpb=4bf5c4a7c42d9d494a088be85bcf6bb38ec6d86b;p=debian%2Fopenrocket

diff --git a/datafiles/thrustcurves/AeroTech_D13.eng b/datafiles/thrustcurves/AeroTech_D13.eng
new file mode 100644
index 00000000..eec171aa
--- /dev/null
+++ b/datafiles/thrustcurves/AeroTech_D13.eng
@@ -0,0 +1,40 @@
+; Aerotech D13 RASP.ENG file made from NAR published data
+; File produced July 4, 2000
+; Submitted to ThrustCurve.org by Chris Kobel (3/29/07)
+; 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.
+D13W   18   70   4-7-10   0.0098   0.0326 AT
+   0.030   13.462
+   0.061   21.171
+   0.085   20.618
+   0.127   21.605
+   0.158   21.042
+   0.182   22.306
+   0.217   22.592
+   0.227   23.610
+   0.248   21.891
+   0.279   23.155
+   0.317   22.039
+   0.366   21.338
+   0.383   21.901
+   0.449   20.648
+   0.462   21.486
+   0.480   19.947
+   0.507   19.947
+   0.521   20.509
+   0.559   18.693
+   0.580   19.118
+   0.660   17.578
+   0.743   15.337
+   0.861   12.406
+   0.947    9.329
+   1.068    5.834
+   1.155    4.158
+   1.172    4.720
+   1.231    2.762
+   1.328    1.928
+   1.404    1.093
+   1.520    0.000