X-Git-Url: https://git.gag.com/?a=blobdiff_plain;f=datafiles%2Fthrustcurves%2FAeroTech_F22.eng;fp=datafiles%2Fthrustcurves%2FAeroTech_F22.eng;h=8cd24a5bb9f627f8b76e0838667a5bc3c2e9bc9b;hb=720d4935bc6bec453e6478ad5227356c626610a2;hp=0000000000000000000000000000000000000000;hpb=4bf5c4a7c42d9d494a088be85bcf6bb38ec6d86b;p=debian%2Fopenrocket diff --git a/datafiles/thrustcurves/AeroTech_F22.eng b/datafiles/thrustcurves/AeroTech_F22.eng new file mode 100644 index 00000000..8cd24a5b --- /dev/null +++ b/datafiles/thrustcurves/AeroTech_F22.eng @@ -0,0 +1,38 @@ +; +;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