git.gag.com Git - debian/openrocket/blob - datafiles/thrustcurves/AeroTech_G40.rse

   1 <engine-database>\r
   2  <engine-list>\r
   3 <engine FDiv="10" FFix="1" FStep="-1." Isp="187.68" Itot="99.02" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="43.052" burn-time="2.3" cgDiv="10" cgFix="1" cgStep="-1." code="G40W" delays="4,7,10" dia="29." exitDia="0." initWt="123." len="124." mDiv="10" mFix="1" mStep="-1." massFrac="43.74" mfg="Aerotech" peakThrust="74.325" propWt="53.8" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
   4 <comments>Aerotech G40W RASP.ENG file made by Tim Van Milligan\r
   5 For RockSim www.RockSim.com\r
   6 File Created March 2, 2005\r
   7 Thrust curve supplied by Aerotech for the molded case G40W motors.\r
   8 </comments>\r
   9 <data>\r
  10 <eng-data cg="62." f="0." m="53.8" t="0."/>\r
  11 <eng-data cg="62." f="74.325" m="53.3154" t="0.024"/>\r
  12 <eng-data cg="62." f="67.005" m="52.0484" t="0.057"/>\r
  13 <eng-data cg="62." f="65.879" m="45.009" t="0.252"/>\r
  14 <eng-data cg="62." f="63.063" m="36.3219" t="0.5"/>\r
  15 <eng-data cg="62." f="60.248" m="27.4447" t="0.765"/>\r
  16 <eng-data cg="62." f="54.054" m="20.1476" t="1."/>\r
  17 <eng-data cg="62." f="47.298" m="13.2642" t="1.25"/>\r
  18 <eng-data cg="62." f="36.599" m="7.52075" t="1.502"/>\r
  19 <eng-data cg="62." f="25.338" m="3.3311" t="1.751"/>\r
  20 <eng-data cg="62." f="12.951" m="0.751488" t="1.999"/>\r
  21 <eng-data cg="62." f="3.941" m="0.191641" t="2.121"/>\r
  22 <eng-data cg="62." f="0." m="0." t="2.3"/>\r
  23 </data>\r
  24 </engine>\r
  25  </engine-list>\r
  26 </engine-database>\r