version 1.0.0
[debian/openrocket] / datafiles / thrustcurves / Apogee_E6.rse
diff --git a/datafiles/thrustcurves/Apogee_E6.rse b/datafiles/thrustcurves/Apogee_E6.rse
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+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="183.39" Itot="38.667" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="6.381" burn-time="6.06" cgDiv="10" cgFix="1" cgStep="-1." code="E6" delays="2,4,6,8,100" dia="24." exitDia="0." initWt="46.3" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="46.44" mfg="Apogee" peakThrust="20.12" propWt="21.5" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech E6 RASP.ENG file made from NAR published data\r
+File produced July 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="35." f="0." m="21.5" t="0."/>\r
+<eng-data cg="35." f="18.59" m="21.2106" t="0.056"/>\r
+<eng-data cg="35." f="20.12" m="20.6079" t="0.112"/>\r
+<eng-data cg="35." f="17.575" m="20.021" t="0.168"/>\r
+<eng-data cg="35." f="14.38" m="18.7862" t="0.307"/>\r
+<eng-data cg="35." f="10.45" m="17.2399" t="0.531"/>\r
+<eng-data cg="35." f="7.696" m="15.4086" t="0.894"/>\r
+<eng-data cg="35." f="6.244" m="14.432" t="1.146"/>\r
+<eng-data cg="35." f="5.808" m="12.6059" t="1.691"/>\r
+<eng-data cg="35." f="5.663" m="8.95436" t="2.836"/>\r
+<eng-data cg="35." f="5.517" m="5.65345" t="3.898"/>\r
+<eng-data cg="35." f="5.227" m="4.52736" t="4.275"/>\r
+<eng-data cg="35." f="4.937" m="4.13176" t="4.415"/>\r
+<eng-data cg="35." f="5.082" m="2.34073" t="5.058"/>\r
+<eng-data cg="35." f="5.227" m="1.01948" t="5.519"/>\r
+<eng-data cg="35." f="6.679" m="0.741439" t="5.603"/>\r
+<eng-data cg="35." f="3.921" m="0.370124" t="5.729"/>\r
+<eng-data cg="35." f="2.323" m="0.104528" t="5.882"/>\r
+<eng-data cg="35." f="1.016" m="0.0265515" t="5.966"/>\r
+<eng-data cg="35." f="0." m="-0." t="6.06"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r