X-Git-Url: https://git.gag.com/?a=blobdiff_plain;f=datafiles%2Fthrustcurves%2FAeroTech_D9.eng;fp=datafiles%2Fthrustcurves%2FAeroTech_D9.eng;h=9d3b607b88d352272cf5a68dce720a4f720dc2d7;hb=720d4935bc6bec453e6478ad5227356c626610a2;hp=0000000000000000000000000000000000000000;hpb=4bf5c4a7c42d9d494a088be85bcf6bb38ec6d86b;p=debian%2Fopenrocket diff --git a/datafiles/thrustcurves/AeroTech_D9.eng b/datafiles/thrustcurves/AeroTech_D9.eng new file mode 100644 index 00000000..9d3b607b --- /dev/null +++ b/datafiles/thrustcurves/AeroTech_D9.eng @@ -0,0 +1,23 @@ +; Aerotech D9 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. +D9W 24 70 4-7 0.0101 0.045 AT + 0.1 13.7 + 0.15 15.4 + 0.2 16.3 + 0.25 16.8 + 0.35 17.2 + 0.40 17.2 + 0.50 16.8 + 0.65 15.9 + 0.80 14.5 + 1.10 9.2 + 1.25 7.0 + 1.40 4.8 + 1.60 2.5 + 1.90 0.0