git.gag.com Git - debian/openrocket/blob - datafiles/thrustcurves/AeroTech_G104.rse

   1 <engine-database>\r
   2  <engine-list>\r
   3 <engine FDiv="10" FFix="1" FStep="-1." Isp="207.1" Itot="82.862" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="92.069" burn-time="0.9" cgDiv="10" cgFix="1" cgStep="-1." code="G104T" delays="6,10,14" dia="29." exitDia="0." initWt="135.6" len="125." mDiv="10" mFix="1" mStep="-1." massFrac="30.09" mfg="Aerotech" peakThrust="118.5" propWt="40.8" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
   4 <data>\r
   5 <eng-data cg="62.5" f="0." m="40.8" t="0."/>\r
   6 <eng-data cg="62.5" f="118.5" m="40.8" t="0."/>\r
   7 <eng-data cg="62.5" f="114.14" m="35.0726" t="0.1"/>\r
   8 <eng-data cg="62.5" f="114.14" m="29.4525" t="0.2"/>\r
   9 <eng-data cg="62.5" f="109.91" m="23.9366" t="0.3"/>\r
  10 <eng-data cg="62.5" f="109.91" m="18.5248" t="0.4"/>\r
  11 <eng-data cg="62.5" f="105.68" m="13.2171" t="0.5"/>\r
  12 <eng-data cg="62.5" f="84.56" m="8.53352" t="0.6"/>\r
  13 <eng-data cg="62.5" f="71.83" m="4.68332" t="0.7"/>\r
  14 <eng-data cg="62.5" f="59.2" m="1.45746" t="0.8"/>\r
  15 <eng-data cg="62.5" f="0." m="0." t="0.9"/>\r
  16 </data>\r
  17 </engine>\r
  18  </engine-list>\r
  19 </engine-database>\r