X-Git-Url: https://git.gag.com/?a=blobdiff_plain;f=datafiles%2Fthrustcurves%2FAeroTech_M1939.eng;fp=datafiles%2Fthrustcurves%2FAeroTech_M1939.eng;h=c012908037e6f36a686bdab9f3e993d06735b870;hb=720d4935bc6bec453e6478ad5227356c626610a2;hp=0000000000000000000000000000000000000000;hpb=4bf5c4a7c42d9d494a088be85bcf6bb38ec6d86b;p=debian%2Fopenrocket diff --git a/datafiles/thrustcurves/AeroTech_M1939.eng b/datafiles/thrustcurves/AeroTech_M1939.eng new file mode 100644 index 00000000..c0129080 --- /dev/null +++ b/datafiles/thrustcurves/AeroTech_M1939.eng @@ -0,0 +1,30 @@ +; AeroTech M1939W +; Copyright Tripoli Motor Testing 1998 (www.tripoli.org) +; provided by ThrustCurve.org (www.thrustcurve.org) +M1939W 98 732 0 5.656 8.98822 AT + 0.134 1905.185 + 0.406 2021.155 + 0.679 2095.900 + 0.952 2158.087 + 1.225 2198.211 + 1.498 2219.694 + 1.770 2228.643 + 2.042 2229.881 + 2.315 2225.641 + 2.587 2211.713 + 2.860 2164.724 + 3.133 2047.014 + 3.405 1916.238 + 3.677 1805.664 + 3.950 1658.489 + 4.223 1497.704 + 4.496 1339.452 + 4.769 1213.061 + 5.041 1102.130 + 5.313 966.508 + 5.585 670.253 + 5.858 443.975 + 6.131 155.355 + 6.404 41.358 + 6.677 5.775 + 6.950 0.000