X-Git-Url: https://git.gag.com/?a=blobdiff_plain;f=datafiles%2Fthrustcurves%2FAeroTech_D15.eng;fp=datafiles%2Fthrustcurves%2FAeroTech_D15.eng;h=c863bf2219fdc15bf2e8336a6240a15ae2d106b0;hb=720d4935bc6bec453e6478ad5227356c626610a2;hp=0000000000000000000000000000000000000000;hpb=4bf5c4a7c42d9d494a088be85bcf6bb38ec6d86b;p=debian%2Fopenrocket diff --git a/datafiles/thrustcurves/AeroTech_D15.eng b/datafiles/thrustcurves/AeroTech_D15.eng new file mode 100644 index 00000000..c863bf22 --- /dev/null +++ b/datafiles/thrustcurves/AeroTech_D15.eng @@ -0,0 +1,26 @@ +; Aerotech D15 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. +D15T 24 70 4-6-8 .0089 .0440 AT + 0.014 11.480 + 0.049 26.272 + 0.081 30.087 + 0.107 31.261 + 0.121 31.249 + 0.159 31.360 + 0.208 31.249 + 0.283 29.583 + 0.439 23.353 + 0.551 18.484 + 0.675 13.430 + 0.863 6.422 + 0.938 3.892 + 1.010 2.335 + 1.085 0.778 + 1.142 0.389 + 1.150 0.000