X-Git-Url: https://git.gag.com/?a=blobdiff_plain;f=datafiles%2Fthrustcurves%2FAeroTech_I225.eng;fp=datafiles%2Fthrustcurves%2FAeroTech_I225.eng;h=ca0504263c423d05bba538e1bcdeff1ee2070498;hb=720d4935bc6bec453e6478ad5227356c626610a2;hp=0000000000000000000000000000000000000000;hpb=4bf5c4a7c42d9d494a088be85bcf6bb38ec6d86b;p=debian%2Fopenrocket

diff --git a/datafiles/thrustcurves/AeroTech_I225.eng b/datafiles/thrustcurves/AeroTech_I225.eng
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+; AeroTech I225FJ
+; Curvefit to instruction sheet on Aerotech website (12/27/06)
+; by Chris Kobel
+; burn time: 1.8 seconds
+; total impulse: 350.5 newton-seconds
+; average thrust: 43.8 pounds
+I225FJ 38 202 6-10-14 0.2417 0.486 AT
+ 0.04	 213.6
+ 0.10	 213.6
+ 0.20	 218.1
+ 0.28	 235.9
+ 0.30	 249.2
+ 0.40	 262.6
+ 0.50	 267.0
+ 0.60	 271.5
+ 0.70	 275.9
+ 0.80	 275.9
+ 0.87	 271.5
+ 0.90	 258.1
+ 1.00	 240.3
+ 1.10	 218.1
+ 1.20	 200.3
+ 1.30	 178.0
+ 1.40	 160.2
+ 1.50	  97.9
+ 1.60	  40.1
+ 1.70	  13.4
+ 1.80	   0.0