version 1.0.0

[debian/openrocket] / datafiles / thrustcurves / AeroTech_F24.rse

diff --git a/datafiles/thrustcurves/AeroTech_F24.rse b/datafiles/thrustcurves/AeroTech_F24.rse
new file mode 100644 (file)
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+++ b/datafiles/thrustcurves/AeroTech_F24.rse
@@ -0,0 +1,42 @@
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="253.89" Itot="47.306" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="22.209" burn-time="2.13" cgDiv="10" cgFix="1" cgStep="-1." code="F24" delays="4,7" dia="24." exitDia="0." initWt="62.5" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="30.4" mfg="Aerotech" peakThrust="40.95" propWt="19." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech F24 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="19." t="0."/>\r
+<eng-data cg="35." f="15.942" m="18.8944" t="0.033"/>\r
+<eng-data cg="35." f="40.146" m="18.0045" t="0.112"/>\r
+<eng-data cg="35." f="40.95" m="17.7928" t="0.125"/>\r
+<eng-data cg="35." f="40.427" m="16.894" t="0.18"/>\r
+<eng-data cg="35." f="40.126" m="15.8425" t="0.245"/>\r
+<eng-data cg="35." f="40.417" m="15.2602" t="0.281"/>\r
+<eng-data cg="35." f="39.524" m="14.0722" t="0.355"/>\r
+<eng-data cg="35." f="39.213" m="12.7598" t="0.438"/>\r
+<eng-data cg="35." f="37.727" m="11.1374" t="0.543"/>\r
+<eng-data cg="35." f="36.532" m="10.2427" t="0.603"/>\r
+<eng-data cg="35." f="33.279" m="9.47159" t="0.658"/>\r
+<eng-data cg="35." f="34.163" m="9.10591" t="0.685"/>\r
+<eng-data cg="35." f="29.434" m="8.58227" t="0.726"/>\r
+<eng-data cg="35." f="29.716" m="8.03586" t="0.772"/>\r
+<eng-data cg="35." f="26.453" m="6.01675" t="0.951"/>\r
+<eng-data cg="35." f="24.666" m="4.78485" t="1.071"/>\r
+<eng-data cg="35." f="22.588" m="4.44323" t="1.107"/>\r
+<eng-data cg="35." f="20.811" m="3.76342" t="1.185"/>\r
+<eng-data cg="35." f="16.644" m="2.27411" t="1.383"/>\r
+<eng-data cg="35." f="10.41" m="0.828926" t="1.649"/>\r
+<eng-data cg="35." f="5.369" m="0.261717" t="1.828"/>\r
+<eng-data cg="35." f="2.403" m="0.0900311" t="1.938"/>\r
+<eng-data cg="35." f="1.806" m="0.0477682" t="1.988"/>\r
+<eng-data cg="35." f="0.912" m="0.0150182" t="2.048"/>\r
+<eng-data cg="35." f="0." m="0." t="2.13"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r