X-Git-Url: https://git.gag.com/?a=blobdiff_plain;f=datafiles%2Fthrustcurves%2FAeroTech_E16.eng;fp=datafiles%2Fthrustcurves%2FAeroTech_E16.eng;h=95afca8faffa53b4555b52727b1ea1a0e8b372ca;hb=720d4935bc6bec453e6478ad5227356c626610a2;hp=0000000000000000000000000000000000000000;hpb=4bf5c4a7c42d9d494a088be85bcf6bb38ec6d86b;p=debian%2Fopenrocket diff --git a/datafiles/thrustcurves/AeroTech_E16.eng b/datafiles/thrustcurves/AeroTech_E16.eng new file mode 100644 index 00000000..95afca8f --- /dev/null +++ b/datafiles/thrustcurves/AeroTech_E16.eng @@ -0,0 +1,32 @@ +; Aerotech E16 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. +E16W 29 124 4-7-10 .0190 .107 AT + 0.132 32.223 + 0.221 37.200 + 0.255 36.699 + 0.306 36.699 + 0.371 35.357 + 0.414 33.785 + 0.437 34.906 + 0.472 33.785 + 0.530 32.894 + 0.553 31.772 + 0.576 32.443 + 0.638 29.309 + 0.720 27.296 + 0.867 23.942 + 1.083 19.245 + 1.273 14.319 + 1.458 9.397 + 1.513 8.055 + 1.524 8.279 + 1.555 6.936 + 1.656 4.474 + 1.814 1.790 + 2.000 0.000