X-Git-Url: https://git.gag.com/?a=blobdiff_plain;f=datafiles%2Fthrustcurves%2FAeroTech_F22.eng;fp=datafiles%2Fthrustcurves%2FAeroTech_F22.eng;h=0000000000000000000000000000000000000000;hb=bf76931b27b597f7bc1dd5a0e7e2460ac065415b;hp=8cd24a5bb9f627f8b76e0838667a5bc3c2e9bc9b;hpb=def27b03bd9ebe6628421ec61112ebe4f45f043d;p=debian%2Fopenrocket

diff --git a/datafiles/thrustcurves/AeroTech_F22.eng b/datafiles/thrustcurves/AeroTech_F22.eng
deleted file mode 100644
index 8cd24a5b..00000000
--- a/datafiles/thrustcurves/AeroTech_F22.eng
+++ /dev/null
@@ -1,38 +0,0 @@
-;
-;Aerotech F22 RASP.ENG file made from NAR published data
-;File produced July 4, 2000
-;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.
-F22 29 125 4-7 0.0463 0.1342 AT
-0.014 11.527
-0.075 20.126
-0.157 26.572
-0.293 29.113
-0.382 30.278
-0.45 29.69
-0.539 30.667
-0.614 30.089
-0.662 31.15
-0.771 30.478
-0.948 29.89
-0.996 28.714
-1.078 28.136
-1.187 27.738
-1.289 26.761
-1.337 26.96
-1.412 25.984
-1.474 25.008
-1.515 26.173
-1.542 24.808
-1.706 22.856
-1.938 20.903
-2.101 18.173
-2.129 19.338
-2.251 16.21
-2.402 13.48
-2.64 8.791
-2.961 3.32
-3.31 0