X-Git-Url: https://git.gag.com/?a=blobdiff_plain;f=datafiles%2Fthrustcurves%2FAeroTech_N2000.eng;fp=datafiles%2Fthrustcurves%2FAeroTech_N2000.eng;h=52788cf53a995a9369c0fbb65f538f9efa0e5b33;hb=720d4935bc6bec453e6478ad5227356c626610a2;hp=0000000000000000000000000000000000000000;hpb=4bf5c4a7c42d9d494a088be85bcf6bb38ec6d86b;p=debian%2Fopenrocket diff --git a/datafiles/thrustcurves/AeroTech_N2000.eng b/datafiles/thrustcurves/AeroTech_N2000.eng new file mode 100644 index 00000000..52788cf5 --- /dev/null +++ b/datafiles/thrustcurves/AeroTech_N2000.eng @@ -0,0 +1,30 @@ +; AeroTech N2000W +; Copyright Tripoli Motor Testing 1997 (www.tripoli.org) +; provided by ThrustCurve.org (www.thrustcurve.org) +N2000W 98 1046 0 7.66707 12.2828 AT + 0.146 2775.075 + 0.446 2831.810 + 0.746 2834.354 + 1.046 2829.564 + 1.346 2777.650 + 1.646 2688.252 + 1.950 2597.973 + 2.254 2501.043 + 2.554 2415.747 + 2.854 2343.624 + 3.154 2262.579 + 3.454 2178.182 + 3.758 2104.164 + 4.062 2024.475 + 4.362 1935.616 + 4.663 1839.781 + 4.962 1756.910 + 5.262 1351.806 + 5.567 954.556 + 5.871 681.831 + 6.171 475.910 + 6.471 361.124 + 6.771 194.633 + 7.071 44.938 + 7.375 6.030 + 7.679 0.000