git.gag.com Git - debian/openrocket/blob - datafiles/thrustcurves/AeroTech_I364.rse

   1 <engine-database>\r
   2  <engine-list>\r
   3 <engine FDiv="10" FFix="1" FStep="-1." Isp="155.05" Itot="551.202" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="324.236" burn-time="1.7" cgDiv="10" cgFix="1" cgStep="-1." code="I364FJ" delays="6,10,14" dia="38." exitDia="0." initWt="678." len="345." mDiv="10" mFix="1" mStep="-1." massFrac="53.47" mfg="Aerotech" peakThrust="413.9" propWt="362.5" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
   4 <comments>AeroTech I364FJ\r
   5 Curvefit to instruction sheet on Aerotech website (12/27/06)\r
   6 by Chris Kobel\r
   7 burn time: 1.7 seconds\r
   8 total impulse: 551.2 newton-seconds\r
   9 average thrust: 72.9 pounds\r
  10 </comments>\r
  11 <data>\r
  12 <eng-data cg="172.5" f="0." m="362.5" t="0."/>\r
  13 <eng-data cg="172.5" f="356." m="360.159" t="0.02"/>\r
  14 <eng-data cg="172.5" f="373.8" m="340.961" t="0.1"/>\r
  15 <eng-data cg="172.5" f="387.2" m="315.937" t="0.2"/>\r
  16 <eng-data cg="172.5" f="400.5" m="290.035" t="0.3"/>\r
  17 <eng-data cg="172.5" f="400.5" m="263.696" t="0.4"/>\r
  18 <eng-data cg="172.5" f="409.4" m="237.064" t="0.5"/>\r
  19 <eng-data cg="172.5" f="413.9" m="209.992" t="0.6"/>\r
  20 <eng-data cg="172.5" f="409.4" m="182.92" t="0.7"/>\r
  21 <eng-data cg="172.5" f="382.7" m="156.873" t="0.8"/>\r
  22 <eng-data cg="172.5" f="373.8" m="131.998" t="0.9"/>\r
  23 <eng-data cg="172.5" f="351.6" m="108.145" t="1."/>\r
  24 <eng-data cg="172.5" f="333.8" m="85.6068" t="1.1"/>\r
  25 <eng-data cg="172.5" f="320.4" m="64.0949" t="1.2"/>\r
  26 <eng-data cg="172.5" f="311.5" m="43.3164" t="1.3"/>\r
  27 <eng-data cg="172.5" f="244.8" m="25.0237" t="1.4"/>\r
  28 <eng-data cg="172.5" f="178." m="11.1209" t="1.5"/>\r
  29 <eng-data cg="172.5" f="80.1" m="2.6339" t="1.6"/>\r
  30 <eng-data cg="172.5" f="0." m="0." t="1.7"/>\r
  31 </data>\r
  32 </engine>\r
  33  </engine-list>\r
  34 </engine-database>\r