X-Git-Url: https://git.gag.com/?a=blobdiff_plain;f=datafiles%2Fthrustcurves%2FAeroTech_I211.eng;fp=datafiles%2Fthrustcurves%2FAeroTech_I211.eng;h=238614cc481adc351b01580c14f733b7be7505c9;hb=720d4935bc6bec453e6478ad5227356c626610a2;hp=0000000000000000000000000000000000000000;hpb=4bf5c4a7c42d9d494a088be85bcf6bb38ec6d86b;p=debian%2Fopenrocket diff --git a/datafiles/thrustcurves/AeroTech_I211.eng b/datafiles/thrustcurves/AeroTech_I211.eng new file mode 100644 index 00000000..238614cc --- /dev/null +++ b/datafiles/thrustcurves/AeroTech_I211.eng @@ -0,0 +1,30 @@ +; AeroTech I211W +; Copyright Tripoli Motor Testing 1999 (www.tripoli.org) +; provided by ThrustCurve.org (www.thrustcurve.org) +I211W 38 240 0 0.247296 0.466368 AT + 0.044 257.326 + 0.134 295.533 + 0.226 296.087 + 0.318 298.204 + 0.408 295.082 + 0.499 287.669 + 0.591 282.578 + 0.682 272.875 + 0.773 266.997 + 0.864 257.602 + 0.955 250.495 + 1.047 238.574 + 1.138 228.571 + 1.228 215.135 + 1.320 198.047 + 1.411 180.631 + 1.502 161.261 + 1.593 146.708 + 1.684 134.484 + 1.776 101.241 + 1.867 52.688 + 1.957 35.461 + 2.049 24.321 + 2.141 11.165 + 2.232 4.587 + 2.324 0.000