version 1.0.0

[debian/openrocket] / datafiles / thrustcurves / AeroTech_E7.rse

diff --git a/datafiles/thrustcurves/AeroTech_E7.rse b/datafiles/thrustcurves/AeroTech_E7.rse
new file mode 100644 (file)
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+++ b/datafiles/thrustcurves/AeroTech_E7.rse
@@ -0,0 +1,42 @@
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="175.03" Itot="29.351" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="5.405" burn-time="5.43" cgDiv="10" cgFix="1" cgStep="-1." code="E7RC" delays="1000" dia="24." exitDia="0." initWt="48.4" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="35.33" mfg="Aerotech" peakThrust="11.58" propWt="17.1" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech E7TRC 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="17.1" t="0."/>\r
+<eng-data cg="35." f="6.636" m="17.0265" t="0.038"/>\r
+<eng-data cg="35." f="10.056" m="16.905" t="0.063"/>\r
+<eng-data cg="35." f="11.019" m="16.7576" t="0.087"/>\r
+<eng-data cg="35." f="11.42" m="16.4504" t="0.134"/>\r
+<eng-data cg="35." f="11.58" m="15.968" t="0.206"/>\r
+<eng-data cg="35." f="11.149" m="15.2662" t="0.312"/>\r
+<eng-data cg="35." f="10.738" m="14.2843" t="0.466"/>\r
+<eng-data cg="35." f="9.777" m="13.0831" t="0.667"/>\r
+<eng-data cg="35." f="8.132" m="11.6589" t="0.94"/>\r
+<eng-data cg="35." f="6.281" m="10.4707" t="1.223"/>\r
+<eng-data cg="35." f="5.182" m="9.59916" t="1.484"/>\r
+<eng-data cg="35." f="4.701" m="8.95139" t="1.709"/>\r
+<eng-data cg="35." f="4.423" m="7.88027" t="2.112"/>\r
+<eng-data cg="35." f="4.279" m="6.19708" t="2.776"/>\r
+<eng-data cg="35." f="4.205" m="4.87734" t="3.31"/>\r
+<eng-data cg="35." f="4.266" m="3.35727" t="3.926"/>\r
+<eng-data cg="35." f="4.192" m="2.18694" t="4.401"/>\r
+<eng-data cg="35." f="4.258" m="1.60356" t="4.638"/>\r
+<eng-data cg="35." f="4.119" m="1.34489" t="4.744"/>\r
+<eng-data cg="35." f="3.979" m="0.448479" t="5.124"/>\r
+<eng-data cg="35." f="3.977" m="0.228306" t="5.219"/>\r
+<eng-data cg="35." f="3.156" m="0.130646" t="5.266"/>\r
+<eng-data cg="35." f="1.992" m="0.0601628" t="5.313"/>\r
+<eng-data cg="35." f="0.965" m="0.0196776" t="5.36"/>\r
+<eng-data cg="35." f="0." m="0." t="5.43"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r