git.gag.com Git - debian/openrocket/blob - core/resources/datafiles/thrustcurves/AeroTech_J340.rse

   1 <engine-database>\r
   2   <engine-list>\r
   3     <engine  mfg="Aerotech" code="J340M" Type="reloadable" dia="38." len="337."\r
   4 initWt="577.3" propWt="365." delays="2,4,6,8,10,14" auto-calc-mass="1"\r
   5 auto-calc-cg="1" avgThrust="298.067" peakThrust="606.518" throatDia="0."\r
   6 exitDia="0." Itot="652.767" burn-time="2.19" massFrac="63.23" Isp="182.37"\r
   7 tDiv="10" tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10"\r
   8 mStep="-1." mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
   9     <comments>AT J340 Metalstorm for 38-720</comments>\r
  10     <data>\r
  11       <eng-data  t="0." f="0." m="365." cg="168.5"/>\r
  12       <eng-data  t="0.005" f="361.55" m="364.495" cg="168.5"/>\r
  13       <eng-data  t="0.008" f="501.742" m="363.771" cg="168.5"/>\r
  14       <eng-data  t="0.026" f="606.518" m="358.193" cg="168.5"/>\r
  15       <eng-data  t="0.096" f="491.412" m="336.706" cg="168.5"/>\r
  16       <eng-data  t="0.214" f="453.044" m="305.548" cg="168.5"/>\r
  17       <eng-data  t="0.485" f="439.762" m="237.904" cg="168.5"/>\r
  18       <eng-data  t="0.772" f="435.335" m="167.687" cg="168.5"/>\r
  19       <eng-data  t="0.826" f="426.481" m="154.676" cg="168.5"/>\r
  20       <eng-data  t="0.891" f="423.53" m="139.229" cg="168.5"/>\r
  21       <eng-data  t="1.048" f="383.685" m="103.797" cg="168.5"/>\r
  22       <eng-data  t="1.389" f="311.375" m="37.5323" cg="168.5"/>\r
  23       <eng-data  t="1.425" f="308.424" m="31.2941" cg="168.5"/>\r
  24       <eng-data  t="1.459" f="309.9" m="25.4165" cg="168.5"/>\r
  25       <eng-data  t="1.554" f="182.988" m="12.3254" cg="168.5"/>\r
  26       <eng-data  t="1.611" f="103.3" m="7.76309" cg="168.5"/>\r
  27       <eng-data  t="1.699" f="57.553" m="3.80562" cg="168.5"/>\r
  28       <eng-data  t="1.841" f="11.806" m="1.05205" cg="168.5"/>\r
  29       <eng-data  t="1.898" f="8.854" m="0.722815" cg="168.5"/>\r
  30       <eng-data  t="2.19" f="0." m="0." cg="168.5"/>\r
  31     </data>\r
  32   </engine>\r
  33 </engine-list>\r
  34 </engine-database>\r