X-Git-Url: https://git.gag.com/?a=blobdiff_plain;f=datafiles%2Fthrustcurves%2FAeroTech_L1120.eng;fp=datafiles%2Fthrustcurves%2FAeroTech_L1120.eng;h=639635ad0cd2261cb6fa2be3ed1612dba174fd87;hb=720d4935bc6bec453e6478ad5227356c626610a2;hp=0000000000000000000000000000000000000000;hpb=4bf5c4a7c42d9d494a088be85bcf6bb38ec6d86b;p=debian%2Fopenrocket

diff --git a/datafiles/thrustcurves/AeroTech_L1120.eng b/datafiles/thrustcurves/AeroTech_L1120.eng
new file mode 100644
index 00000000..639635ad
--- /dev/null
+++ b/datafiles/thrustcurves/AeroTech_L1120.eng
@@ -0,0 +1,30 @@
+; AeroTech L1120W
+; Copyright Tripoli Motor Testing 1998 (www.tripoli.org)
+; provided by ThrustCurve.org (www.thrustcurve.org)
+L1120W 75 665 0 2.75699 4.65786 AT
+   0.097 1377.215
+   0.293 1442.670
+   0.489 1496.986
+   0.685 1537.057
+   0.882 1554.962
+   1.078 1554.131
+   1.275 1547.973
+   1.472 1533.465
+   1.668 1510.342
+   1.865 1472.279
+   2.061 1362.534
+   2.257 1245.425
+   2.454 1148.864
+   2.651 1062.680
+   2.847 984.952
+   3.044 916.169
+   3.241 831.929
+   3.436 766.450
+   3.633 698.978
+   3.830 562.966
+   4.026 384.579
+   4.223 227.654
+   4.420 105.078
+   4.616 56.339
+   4.813 21.712
+   5.009 0.000