version 1.0.0

[debian/openrocket] / datafiles / thrustcurves / AeroTech_H250.rse

diff --git a/datafiles/thrustcurves/AeroTech_H250.rse b/datafiles/thrustcurves/AeroTech_H250.rse
new file mode 100644 (file)
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+++ b/datafiles/thrustcurves/AeroTech_H250.rse
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+<engine-database>\r
+  <engine-list>\r
+    <engine  mfg="Aerotech" code="H250G" Type="reloadable" dia="29." len="228.93"\r
+initWt="256." propWt="116.3" delays="0,6,10,14" auto-calc-mass="1"\r
+auto-calc-cg="1" avgThrust="251.105" peakThrust="320.655" throatDia="0."\r
+exitDia="0." Itot="231.017" burn-time="0.92" massFrac="0." Isp="0." tDiv="10"\r
+tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
+mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
+    <comments>I don't know that \r
+these ejection \r
+delays are correct.  \r
+This was made \r
+using the Aerotech \r
+test thrust curves.  \r
+By Tobin Yehle, \r
+11/11/07.</comments>\r
+    <data>\r
+      <eng-data  t="0." f="0." m="0." cg="0."/>\r
+      <eng-data  t="0.00250627" f="88.6915" m="0." cg="0."/>\r
+      <eng-data  t="0.0125313" f="177.383" m="0." cg="0."/>\r
+      <eng-data  t="0.0300752" f="279.719" m="0." cg="0."/>\r
+      <eng-data  t="0.0726817" f="311.103" m="0." cg="0."/>\r
+      <eng-data  t="0.145363" f="320.654" m="0." cg="0."/>\r
+      <eng-data  t="0.24812" f="311.103" m="0." cg="0."/>\r
+      <eng-data  t="0.308271" f="297.458" m="0." cg="0."/>\r
+      <eng-data  t="0.398496" f="282.448" m="0." cg="0."/>\r
+      <eng-data  t="0.45614" f="270.168" m="0." cg="0."/>\r
+      <eng-data  t="0.593985" f="238.785" m="0." cg="0."/>\r
+      <eng-data  t="0.691729" f="221.047" m="0." cg="0."/>\r
+      <eng-data  t="0.799499" f="218.318" m="0." cg="0."/>\r
+      <eng-data  t="0.83208" f="210.131" m="0." cg="0."/>\r
+      <eng-data  t="0.844612" f="189.663" m="0." cg="0."/>\r
+      <eng-data  t="0.907268" f="13.6449" m="0." cg="0."/>\r
+      <eng-data  t="0.92" f="0." m="0." cg="0."/>\r
+    </data>\r
+  </engine>\r
+</engine-list>\r
+</engine-database>\r