version 1.0.0
[debian/openrocket] / datafiles / thrustcurves / AeroTech_E23.rse
diff --git a/datafiles/thrustcurves/AeroTech_E23.rse b/datafiles/thrustcurves/AeroTech_E23.rse
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+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="207.01" Itot="35.323" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="22.498" burn-time="1.57" cgDiv="10" cgFix="1" cgStep="-1." code="E23" delays="5,8" dia="29." exitDia="0." initWt="103.9" len="124." mDiv="10" mFix="1" mStep="-1." massFrac="16.75" mfg="Aerotech" peakThrust="38.22" propWt="17.4" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech E23 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="62." f="0." m="17.4" t="0."/>\r
+<eng-data cg="62." f="16.299" m="17.3037" t="0.024"/>\r
+<eng-data cg="62." f="21.959" m="17.2" t="0.035"/>\r
+<eng-data cg="62." f="30.785" m="16.7843" t="0.067"/>\r
+<eng-data cg="62." f="35.774" m="16.4072" t="0.09"/>\r
+<eng-data cg="62." f="37.577" m="15.2691" t="0.153"/>\r
+<eng-data cg="62." f="38.22" m="14.3916" t="0.2"/>\r
+<eng-data cg="62." f="37.357" m="13.647" t="0.24"/>\r
+<eng-data cg="62." f="37.577" m="12.1336" t="0.322"/>\r
+<eng-data cg="62." f="35.093" m="10.8628" t="0.393"/>\r
+<eng-data cg="62." f="32.378" m="8.51964" t="0.534"/>\r
+<eng-data cg="62." f="27.168" m="5.68905" t="0.727"/>\r
+<eng-data cg="62." f="26.938" m="5.16932" t="0.766"/>\r
+<eng-data cg="62." f="25.125" m="4.75898" t="0.798"/>\r
+<eng-data cg="62." f="21.729" m="3.48956" t="0.908"/>\r
+<eng-data cg="62." f="16.98" m="2.06898" t="1.057"/>\r
+<eng-data cg="62." f="12.682" m="1.11923" t="1.187"/>\r
+<eng-data cg="62." f="7.471" m="0.379638" t="1.336"/>\r
+<eng-data cg="62." f="3.169" m="0.0808848" t="1.45"/>\r
+<eng-data cg="62." f="1.584" m="0.0258633" t="1.497"/>\r
+<eng-data cg="62." f="0.679" m="0.00635506" t="1.532"/>\r
+<eng-data cg="62." f="0." m="0." t="1.57"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r