git.gag.com Git - debian/openrocket/blob - datafiles/thrustcurves/AeroTech_H250.rse

   1 <engine-database>\r
   2   <engine-list>\r
   3     <engine  mfg="Aerotech" code="H250G" Type="reloadable" dia="29." len="228.93"\r
   4 initWt="256." propWt="116.3" delays="0,6,10,14" auto-calc-mass="1"\r
   5 auto-calc-cg="1" avgThrust="251.105" peakThrust="320.655" throatDia="0."\r
   6 exitDia="0." Itot="231.017" burn-time="0.92" massFrac="0." Isp="0." tDiv="10"\r
   7 tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
   8 mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
   9     <comments>I don't know that \r
  10 these ejection \r
  11 delays are correct.  \r
  12 This was made \r
  13 using the Aerotech \r
  14 test thrust curves.  \r
  15 By Tobin Yehle, \r
  16 11/11/07.</comments>\r
  17     <data>\r
  18       <eng-data  t="0." f="0." m="0." cg="0."/>\r
  19       <eng-data  t="0.00250627" f="88.6915" m="0." cg="0."/>\r
  20       <eng-data  t="0.0125313" f="177.383" m="0." cg="0."/>\r
  21       <eng-data  t="0.0300752" f="279.719" m="0." cg="0."/>\r
  22       <eng-data  t="0.0726817" f="311.103" m="0." cg="0."/>\r
  23       <eng-data  t="0.145363" f="320.654" m="0." cg="0."/>\r
  24       <eng-data  t="0.24812" f="311.103" m="0." cg="0."/>\r
  25       <eng-data  t="0.308271" f="297.458" m="0." cg="0."/>\r
  26       <eng-data  t="0.398496" f="282.448" m="0." cg="0."/>\r
  27       <eng-data  t="0.45614" f="270.168" m="0." cg="0."/>\r
  28       <eng-data  t="0.593985" f="238.785" m="0." cg="0."/>\r
  29       <eng-data  t="0.691729" f="221.047" m="0." cg="0."/>\r
  30       <eng-data  t="0.799499" f="218.318" m="0." cg="0."/>\r
  31       <eng-data  t="0.83208" f="210.131" m="0." cg="0."/>\r
  32       <eng-data  t="0.844612" f="189.663" m="0." cg="0."/>\r
  33       <eng-data  t="0.907268" f="13.6449" m="0." cg="0."/>\r
  34       <eng-data  t="0.92" f="0." m="0." cg="0."/>\r
  35     </data>\r
  36   </engine>\r
  37 </engine-list>\r
  38 </engine-database>\r