git.gag.com Git - debian/openrocket/blob - datafiles/thrustcurves/AeroTech_M2030.rse

   1 <engine-database>\r
   2   <engine-list>\r
   3     <engine  mfg="Aerotech" code="M2030G" Type="reloadable" dia="75." len="653."\r
   4 initWt="4906." propWt="2663." delays="1000" auto-calc-mass="1" auto-calc-cg="1"\r
   5 avgThrust="2002.58" peakThrust="2645.93" throatDia="0." exitDia="0."\r
   6 Itot="5356.89" burn-time="2.67" massFrac="54.28" Isp="205.13" 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>Took this data from the Aerotech Typical Time-Thrust Curve that comes with the M2030G motor.</comments>\r
  10     <data>\r
  11       <eng-data  t="0." f="0." m="2663." cg="326.5"/>\r
  12       <eng-data  t="0.00776398" f="1342.14" m="2660.41" cg="326.5"/>\r
  13       <eng-data  t="0.0776398" f="2147.42" m="2599.8" cg="326.5"/>\r
  14       <eng-data  t="0.15528" f="1840.64" m="2522.84" cg="326.5"/>\r
  15       <eng-data  t="0.496894" f="2224.11" m="2177.7" cg="326.5"/>\r
  16       <eng-data  t="0.784161" f="2607.58" m="1832.7" cg="326.5"/>\r
  17       <eng-data  t="1.00155" f="2645.93" m="1548.83" cg="326.5"/>\r
  18       <eng-data  t="1.3587" f="2530.88" m="1089.28" cg="326.5"/>\r
  19       <eng-data  t="1.49068" f="2415.84" m="926.996" cg="326.5"/>\r
  20       <eng-data  t="1.99534" f="1802.3" m="397.884" cg="326.5"/>\r
  21       <eng-data  t="2.3913" f="1418.83" m="80.8616" cg="326.5"/>\r
  22       <eng-data  t="2.5" f="805.282" m="20.7723" cg="326.5"/>\r
  23       <eng-data  t="2.56211" f="191.734" m="5.37992" cg="326.5"/>\r
  24       <eng-data  t="2.675" f="0." m="0." cg="326.5"/>\r
  25     </data>\r
  26   </engine>\r
  27 </engine-list>\r
  28 </engine-database>\r