version 1.0.0

[debian/openrocket] / datafiles / thrustcurves / AeroTech_G64.rse

diff --git a/datafiles/thrustcurves/AeroTech_G64.rse b/datafiles/thrustcurves/AeroTech_G64.rse
new file mode 100644 (file)
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+++ b/datafiles/thrustcurves/AeroTech_G64.rse
@@ -0,0 +1,46 @@
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="193.83" Itot="118.803" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="56.844" burn-time="2.09" cgDiv="10" cgFix="1" cgStep="-1." code="G64" delays="4,8,10" dia="29." exitDia="0." initWt="151.2" len="124." mDiv="10" mFix="1" mStep="-1." massFrac="41.34" mfg="Aerotech" peakThrust="98.31" propWt="62.5" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech G64 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="62.5" t="0."/>\r
+<eng-data cg="62." f="54.325" m="62.2999" t="0.014"/>\r
+<eng-data cg="62." f="81.488" m="61.6569" t="0.032"/>\r
+<eng-data cg="62." f="98.31" m="60.38" t="0.059"/>\r
+<eng-data cg="62." f="85.021" m="58.3546" t="0.101"/>\r
+<eng-data cg="62." f="83.847" m="55.5117" t="0.165"/>\r
+<eng-data cg="62." f="85.614" m="50.6531" t="0.274"/>\r
+<eng-data cg="62." f="87.39" m="46.2844" t="0.37"/>\r
+<eng-data cg="62." f="86.798" m="41.4276" t="0.476"/>\r
+<eng-data cg="62." f="91.516" m="40.1612" t="0.503"/>\r
+<eng-data cg="62." f="85.614" m="39.5089" t="0.517"/>\r
+<eng-data cg="62." f="83.847" m="36.4778" t="0.585"/>\r
+<eng-data cg="62." f="80.896" m="30.4977" t="0.723"/>\r
+<eng-data cg="62." f="82.07" m="29.5546" t="0.745"/>\r
+<eng-data cg="62." f="77.945" m="28.3761" t="0.773"/>\r
+<eng-data cg="62." f="75.576" m="23.9341" t="0.883"/>\r
+<eng-data cg="62." f="74.401" m="19.7918" t="0.988"/>\r
+<eng-data cg="62." f="69.673" m="15.8126" t="1.093"/>\r
+<eng-data cg="62." f="61.412" m="9.98534" t="1.262"/>\r
+<eng-data cg="62." f="61.994" m="9.40105" t="1.28"/>\r
+<eng-data cg="62." f="58.451" m="7.94368" t="1.326"/>\r
+<eng-data cg="62." f="54.907" m="6.57206" t="1.372"/>\r
+<eng-data cg="62." f="47.238" m="5.22865" t="1.422"/>\r
+<eng-data cg="62." f="34.841" m="3.43667" t="1.505"/>\r
+<eng-data cg="62." f="23.027" m="2.12761" t="1.591"/>\r
+<eng-data cg="62." f="13.581" m="1.06837" t="1.701"/>\r
+<eng-data cg="62." f="7.085" m="0.372564" t="1.829"/>\r
+<eng-data cg="62." f="4.133" m="0.157156" t="1.902"/>\r
+<eng-data cg="62." f="1.771" m="0.0577648" t="1.966"/>\r
+<eng-data cg="62." f="0." m="0." t="2.09"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r