version 1.0.0

[debian/openrocket] / datafiles / thrustcurves / AeroTech_I211.rse

diff --git a/datafiles/thrustcurves/AeroTech_I211.rse b/datafiles/thrustcurves/AeroTech_I211.rse
new file mode 100644 (file)
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+++ b/datafiles/thrustcurves/AeroTech_I211.rse
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+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="179.66" Itot="440.462" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="200.21" burn-time="2.2" cgDiv="10" cgFix="1" cgStep="-1." code="I211W" delays="6,10,14" dia="38." exitDia="0." initWt="476.3" len="250." mDiv="10" mFix="1" mStep="-1." massFrac="52.49" mfg="Aerotech" peakThrust="386." propWt="250." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="125." f="0." m="250." t="0."/>\r
+<eng-data cg="125." f="386." m="250." t="0."/>\r
+<eng-data cg="125." f="289.39" m="230.833" t="0.1"/>\r
+<eng-data cg="125." f="276.22" m="214.781" t="0.2"/>\r
+<eng-data cg="125." f="276.22" m="199.103" t="0.3"/>\r
+<eng-data cg="125." f="293.79" m="182.927" t="0.4"/>\r
+<eng-data cg="125." f="271.86" m="166.874" t="0.5"/>\r
+<eng-data cg="125." f="271.86" m="151.444" t="0.6"/>\r
+<eng-data cg="125." f="206.08" m="56.4989" t="1.3"/>\r
+<eng-data cg="125." f="131.57" m="8.58756" t="1.8"/>\r
+<eng-data cg="125." f="52.62" m="3.36039" t="1.9"/>\r
+<eng-data cg="125." f="21.93" m="1.24471" t="2."/>\r
+<eng-data cg="125." f="0." m="0." t="2.2"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r