X-Git-Url: https://git.gag.com/?a=blobdiff_plain;f=datafiles%2Fthrustcurves%2FAeroTech_F35.eng;fp=datafiles%2Fthrustcurves%2FAeroTech_F35.eng;h=6f00123dd25428065d1a3d0a93ef8241c0bce3d9;hb=720d4935bc6bec453e6478ad5227356c626610a2;hp=0000000000000000000000000000000000000000;hpb=4bf5c4a7c42d9d494a088be85bcf6bb38ec6d86b;p=debian%2Fopenrocket diff --git a/datafiles/thrustcurves/AeroTech_F35.eng b/datafiles/thrustcurves/AeroTech_F35.eng new file mode 100644 index 00000000..6f00123d --- /dev/null +++ b/datafiles/thrustcurves/AeroTech_F35.eng @@ -0,0 +1,34 @@ +; Curve fit of AT Instruction Sheet by C. Kobel 7/29/08 +F35W 24 95 5-8-11 0.03 0.085 AT + 0.007 39.452 + 0.012 51.842 + 0.019 49.885 + 0.034 57.873 + 0.048 58.363 + 0.058 57.221 + 0.077 54.45 + 0.098 54.939 + 0.106 53.961 + 0.201 53.472 + 0.299 53.309 + 0.398 52.005 + 0.498 52.005 + 0.549 49.559 + 0.601 48.907 + 0.653 47.277 + 0.702 45.647 + 0.752 44.669 + 0.802 43.201 + 0.898 39.778 + 0.946 39.615 + 0.984 36.843 + 1.003 37.332 + 1.102 33.583 + 1.144 30.159 + 1.200 22.334 + 1.298 10.923 + 1.346 6.521 + 1.398 3.260 + 1.448 1.793 + 1.497 0.978 + 1.600 0.0