version 1.0.0

[debian/openrocket] / datafiles / thrustcurves / AeroTech_I305.rse

diff --git a/datafiles/thrustcurves/AeroTech_I305.rse b/datafiles/thrustcurves/AeroTech_I305.rse
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+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="149.89" Itot="443.903" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="277.44" burn-time="1.6" cgDiv="10" cgFix="1" cgStep="-1." code="I305FJ" delays="6,10,14" dia="38." exitDia="0." initWt="581." len="298." mDiv="10" mFix="1" mStep="-1." massFrac="51.98" mfg="Aerotech" peakThrust="405.662" propWt="302." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>I305FJ based on Aerotech instruction sheet by C. Kobel 3/30/07</comments>\r
+<data>\r
+<eng-data cg="149." f="0." m="302." t="0."/>\r
+<eng-data cg="149." f="341.398" m="299.677" t="0.02"/>\r
+<eng-data cg="149." f="365.497" m="280.441" t="0.1"/>\r
+<eng-data cg="149." f="383.571" m="254.96" t="0.2"/>\r
+<eng-data cg="149." f="403.653" m="228.181" t="0.3"/>\r
+<eng-data cg="149." f="405.662" m="200.651" t="0.4"/>\r
+<eng-data cg="149." f="405.662" m="173.053" t="0.5"/>\r
+<eng-data cg="149." f="404.657" m="145.489" t="0.6"/>\r
+<eng-data cg="149." f="374.534" m="118.984" t="0.7"/>\r
+<eng-data cg="149." f="342.402" m="94.596" t="0.8"/>\r
+<eng-data cg="149." f="309.267" m="72.4285" t="0.9"/>\r
+<eng-data cg="149." f="272.115" m="52.652" t="1."/>\r
+<eng-data cg="149." f="238.979" m="35.2664" t="1.1"/>\r
+<eng-data cg="149." f="224.921" m="27.3763" t="1.15"/>\r
+<eng-data cg="149." f="194.798" m="20.2376" t="1.2"/>\r
+<eng-data cg="149." f="119.489" m="9.54671" t="1.3"/>\r
+<eng-data cg="149." f="62.255" m="3.36443" t="1.4"/>\r
+<eng-data cg="149." f="33.136" m="1.742" t="1.45"/>\r
+<eng-data cg="149." f="23.095" m="0.785609" t="1.5"/>\r
+<eng-data cg="149." f="0." m="0." t="1.6"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r