version 1.0.0

[debian/openrocket] / datafiles / thrustcurves / AeroTech_F25.rse

diff --git a/datafiles/thrustcurves/AeroTech_F25.rse b/datafiles/thrustcurves/AeroTech_F25.rse
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+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="185.98" Itot="70.767" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="26.307" burn-time="2.69" cgDiv="10" cgFix="1" cgStep="-1." code="F25" delays="4,6,9" dia="29." exitDia="0." initWt="97.2" len="98." mDiv="10" mFix="1" mStep="-1." massFrac="39.92" mfg="Aerotech" peakThrust="57.631" propWt="38.8" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>F25 Motor Thrust Curve created by Tim Van Milligan\r
+for RockSim Users - www.rocksim.com\r
+file produced March 2, 2005\r
+Based on data supplied by Aerotech for the newer molded case F25.\r
+</comments>\r
+<data>\r
+<eng-data cg="49." f="0." m="38.8" t="0."/>\r
+<eng-data cg="49." f="57.631" m="38.1838" t="0.039"/>\r
+<eng-data cg="49." f="53.491" m="33.6753" t="0.187"/>\r
+<eng-data cg="49." f="51.239" m="29.2252" t="0.342"/>\r
+<eng-data cg="49." f="47.86" m="24.9328" t="0.5"/>\r
+<eng-data cg="49." f="33.806" m="13.7388" t="1."/>\r
+<eng-data cg="49." f="22.94" m="5.96068" t="1.5"/>\r
+<eng-data cg="49." f="10.135" m="1.42709" t="2."/>\r
+<eng-data cg="49." f="4.504" m="0.596372" t="2.207"/>\r
+<eng-data cg="49." f="0." m="0." t="2.69"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r