version 1.0.0

[debian/openrocket] / datafiles / thrustcurves / AeroTech_I195.rse

diff --git a/datafiles/thrustcurves/AeroTech_I195.rse b/datafiles/thrustcurves/AeroTech_I195.rse
new file mode 100644 (file)
index 0000000..4bc0e4e
--- /dev/null
+++ b/datafiles/thrustcurves/AeroTech_I195.rse
@@ -0,0 +1,28 @@
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="148.54" Itot="455.2" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="160.848" burn-time="2.83" cgDiv="10" cgFix="1" cgStep="-1." code="I195J" delays="6,10,14" dia="38." exitDia="0." initWt="582.4" len="297." mDiv="10" mFix="1" mStep="-1." massFrac="53.66" mfg="Aerotech" peakThrust="244.78" propWt="312.5" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="148.5" f="0." m="312.5" t="0."/>\r
+<eng-data cg="148.5" f="244.78" m="312.5" t="0."/>\r
+<eng-data cg="148.5" f="236.61" m="295.976" t="0.1"/>\r
+<eng-data cg="148.5" f="216.19" m="280.433" t="0.2"/>\r
+<eng-data cg="148.5" f="212.11" m="265.732" t="0.3"/>\r
+<eng-data cg="148.5" f="212.11" m="105.554" t="1.4"/>\r
+<eng-data cg="148.5" f="203.94" m="91.2728" t="1.5"/>\r
+<eng-data cg="148.5" f="188.46" m="77.8035" t="1.6"/>\r
+<eng-data cg="148.5" f="179.49" m="65.1734" t="1.7"/>\r
+<eng-data cg="148.5" f="156.65" m="53.6352" t="1.8"/>\r
+<eng-data cg="148.5" f="142.78" m="43.357" t="1.9"/>\r
+<eng-data cg="148.5" f="130.53" m="33.9755" t="2."/>\r
+<eng-data cg="148.5" f="118.28" m="25.435" t="2.1"/>\r
+<eng-data cg="148.5" f="106.08" m="17.7337" t="2.2"/>\r
+<eng-data cg="148.5" f="89.74" m="11.012" t="2.3"/>\r
+<eng-data cg="148.5" f="63.63" m="5.74751" t="2.4"/>\r
+<eng-data cg="148.5" f="32.62" m="2.44367" t="2.5"/>\r
+<eng-data cg="148.5" f="8.97" m="1.01607" t="2.6"/>\r
+<eng-data cg="148.5" f="8.97" m="0.400271" t="2.7"/>\r
+<eng-data cg="148.5" f="0." m="0." t="2.83"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r