X-Git-Url: https://git.gag.com/?a=blobdiff_plain;f=datafiles%2Fthrustcurves%2FAeroTech_E15_1.eng;fp=datafiles%2Fthrustcurves%2FAeroTech_E15_1.eng;h=0000000000000000000000000000000000000000;hb=bf76931b27b597f7bc1dd5a0e7e2460ac065415b;hp=2bd38b28d7c20117429c3570a3cb7d7dedd6c759;hpb=def27b03bd9ebe6628421ec61112ebe4f45f043d;p=debian%2Fopenrocket

diff --git a/datafiles/thrustcurves/AeroTech_E15_1.eng b/datafiles/thrustcurves/AeroTech_E15_1.eng
deleted file mode 100644
index 2bd38b28..00000000
--- a/datafiles/thrustcurves/AeroTech_E15_1.eng
+++ /dev/null
@@ -1,41 +0,0 @@
-; Aerotech E15 RASP.ENG file made from NAR published data
-; File produced July 4, 2000
-; Submitted to ThrustCurve.org by Chris Kobel (3/30/07)
-; 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.
-E15W 24 70 4-7 .0201 .0501 AT
-   0.020 23.330
-   0.036 27.318
-   0.058 28.840
-   0.079 27.171
-   0.139 25.638
-   0.183 24.263
-   0.237 24.106
-   0.297 22.426
-   0.373 21.964
-   0.400 20.894
-   0.443 21.355
-   0.487 20.442
-   0.617 19.833
-   0.742 18.457
-   0.812 20.000
-   0.850 18.006
-   0.899 18.467
-   1.035 17.711
-   1.100 16.945
-   1.160 16.945
-   1.377 15.736
-   1.426 14.656
-   1.436 16.198
-   1.463 14.813
-   1.550 14.361
-   1.572 15.432
-   1.610 13.752
-   1.827 12.839
-   2.126 10.098
-   2.337 6.116
-   2.538 1.369
-   2.600 0.000