version 1.0.0
[debian/openrocket] / datafiles / thrustcurves / AeroTech_F52.rse
diff --git a/datafiles/thrustcurves/AeroTech_F52.rse b/datafiles/thrustcurves/AeroTech_F52.rse
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+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="203.25" Itot="72.95" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="51.374" burn-time="1.42" cgDiv="10" cgFix="1" cgStep="-1." code="F52" delays="5,8,11" dia="29." exitDia="0." initWt="121.4" len="124." mDiv="10" mFix="1" mStep="-1." massFrac="30.15" mfg="Aerotech" peakThrust="78.95" propWt="36.6" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech F52 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="36.6" t="0."/>\r
+<eng-data cg="62." f="46.899" m="36.4588" t="0.012"/>\r
+<eng-data cg="62." f="61.778" m="35.8863" t="0.033"/>\r
+<eng-data cg="62." f="69.441" m="35.1292" t="0.056"/>\r
+<eng-data cg="62." f="73.483" m="33.6592" t="0.097"/>\r
+<eng-data cg="62." f="76.636" m="32.9814" t="0.115"/>\r
+<eng-data cg="62." f="74.381" m="32.4131" t="0.13"/>\r
+<eng-data cg="62." f="74.82" m="31.5523" t="0.153"/>\r
+<eng-data cg="62." f="78.422" m="30.9757" t="0.168"/>\r
+<eng-data cg="62." f="78.95" m="30.423" t="0.182"/>\r
+<eng-data cg="62." f="77.963" m="29.4783" t="0.206"/>\r
+<eng-data cg="62." f="77.504" m="28.2303" t="0.238"/>\r
+<eng-data cg="62." f="73.892" m="27.4707" t="0.258"/>\r
+<eng-data cg="62." f="72.974" m="25.4076" t="0.314"/>\r
+<eng-data cg="62." f="72.046" m="22.6428" t="0.39"/>\r
+<eng-data cg="62." f="70.679" m="21.2822" t="0.428"/>\r
+<eng-data cg="62." f="65.699" m="18.7848" t="0.501"/>\r
+<eng-data cg="62." f="62.975" m="16.719" t="0.565"/>\r
+<eng-data cg="62." f="58.874" m="12.9593" t="0.688"/>\r
+<eng-data cg="62." f="56.15" m="11.1992" t="0.749"/>\r
+<eng-data cg="62." f="52.517" m="8.80035" t="0.837"/>\r
+<eng-data cg="62." f="49.793" m="7.15779" t="0.901"/>\r
+<eng-data cg="62." f="46.161" m="5.47285" t="0.971"/>\r
+<eng-data cg="62." f="39.365" m="2.96266" t="1.088"/>\r
+<eng-data cg="62." f="34.386" m="1.92661" t="1.144"/>\r
+<eng-data cg="62." f="29.417" m="1.46246" t="1.173"/>\r
+<eng-data cg="62." f="20.376" m="0.850406" t="1.222"/>\r
+<eng-data cg="62." f="13.151" m="0.404654" t="1.275"/>\r
+<eng-data cg="62." f="5.461" m="0.105843" t="1.339"/>\r
+<eng-data cg="62." f="1.838" m="0.0142932" t="1.389"/>\r
+<eng-data cg="62." f="0." m="0." t="1.42"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r