version 1.0.0

[debian/openrocket] / datafiles / thrustcurves / AeroTech_G71.rse

diff --git a/datafiles/thrustcurves/AeroTech_G71.rse b/datafiles/thrustcurves/AeroTech_G71.rse
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+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="191.57" Itot="106.894" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="62.879" burn-time="1.7" cgDiv="10" cgFix="1" cgStep="-1." code="G71R" delays="4,7,10" dia="29." exitDia="0." initWt="147." len="124." mDiv="10" mFix="1" mStep="-1." massFrac="38.71" mfg="Aerotech" peakThrust="117.884" propWt="56.9" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>G71R based on Aerotech instruction sheet by C. Kobel 3/29/07</comments>\r
+<data>\r
+<eng-data cg="62." f="0." m="56.9" t="0."/>\r
+<eng-data cg="62." f="0.389" m="56.9" t="0."/>\r
+<eng-data cg="62." f="109.714" m="55.4348" t="0.05"/>\r
+<eng-data cg="62." f="117.884" m="52.406" t="0.1"/>\r
+<eng-data cg="62." f="113.216" m="46.2552" t="0.2"/>\r
+<eng-data cg="62." f="109.714" m="40.3219" t="0.3"/>\r
+<eng-data cg="62." f="105.045" m="34.606" t="0.4"/>\r
+<eng-data cg="62." f="99.21" m="29.1697" t="0.5"/>\r
+<eng-data cg="62." f="92.207" m="24.0751" t="0.6"/>\r
+<eng-data cg="62." f="83.258" m="19.405" t="0.7"/>\r
+<eng-data cg="62." f="75.477" m="15.1803" t="0.8"/>\r
+<eng-data cg="62." f="68.085" m="11.3593" t="0.9"/>\r
+<eng-data cg="62." f="57.97" m="8.00433" t="1."/>\r
+<eng-data cg="62." f="47.465" m="5.19815" t="1.1"/>\r
+<eng-data cg="62." f="33.848" m="3.03398" t="1.2"/>\r
+<eng-data cg="62." f="21.009" m="1.57395" t="1.3"/>\r
+<eng-data cg="62." f="11.283" m="0.714487" t="1.4"/>\r
+<eng-data cg="62." f="5.447" m="0.269213" t="1.5"/>\r
+<eng-data cg="62." f="2.334" m="0.06212" t="1.6"/>\r
+<eng-data cg="62." f="0." m="0." t="1.7"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r