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[debian/openrocket] / datafiles / thrustcurves / AeroTech_I225.eng

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