X-Git-Url: https://git.gag.com/?a=blobdiff_plain;f=datafiles%2Fthrustcurves%2FAeroTech_H55.eng;fp=datafiles%2Fthrustcurves%2FAeroTech_H55.eng;h=579bd6a4bc64363547081fd07de5e7226724d698;hb=720d4935bc6bec453e6478ad5227356c626610a2;hp=0000000000000000000000000000000000000000;hpb=4bf5c4a7c42d9d494a088be85bcf6bb38ec6d86b;p=debian%2Fopenrocket diff --git a/datafiles/thrustcurves/AeroTech_H55.eng b/datafiles/thrustcurves/AeroTech_H55.eng new file mode 100644 index 00000000..579bd6a4 --- /dev/null +++ b/datafiles/thrustcurves/AeroTech_H55.eng @@ -0,0 +1,30 @@ +; AeroTech H55W +; Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +; provided by ThrustCurve.org (www.thrustcurve.org) +H55W 29 191 0 0.09856 0.18816 AT + 0.052 92.752 + 0.159 98.019 + 0.268 95.821 + 0.375 96.162 + 0.482 97.146 + 0.591 96.927 + 0.699 95.915 + 0.806 94.447 + 0.914 92.001 + 1.022 88.756 + 1.129 86.970 + 1.236 84.072 + 1.345 80.172 + 1.453 74.343 + 1.560 64.990 + 1.668 46.380 + 1.776 32.835 + 1.883 25.734 + 1.991 19.920 + 2.099 16.229 + 2.207 13.059 + 2.315 10.451 + 2.422 7.700 + 2.530 5.696 + 2.639 3.979 + 2.747 0.000