git.gag.com Git - debian/openrocket/blob - datafiles/thrustcurves/Cesaroni_I216.rse

   1 <engine-database>\r
   2   <engine-list>\r
   3     <engine  mfg="CTI" code="I216-CL(I)" Type="reloadable" dia="38." len="367." initWt="601."\r
   4 propWt="312.5" delays="5,7,9,11,14" auto-calc-mass="1" auto-calc-cg="1"\r
   5 avgThrust="205.198" peakThrust="345." throatDia="0." exitDia="0." Itot="636.114"\r
   6 burn-time="3.1" massFrac="52." Isp="207.57" tDiv="10" tStep="-1." tFix="1"\r
   7 FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"\r
   8 cgStep="-1." cgFix="1">\r
   9     <comments>This motor is a standard Pro38-5G with a different nozzle to keep total impulse in 'I' range</comments>\r
  10     <data>\r
  11       <eng-data  t="0." f="0." m="312.5" cg="183.5"/>\r
  12       <eng-data  t="0.017" f="35." m="312.354" cg="183.5"/>\r
  13       <eng-data  t="0.03" f="300." m="311.284" cg="183.5"/>\r
  14       <eng-data  t="0.035" f="345." m="310.492" cg="183.5"/>\r
  15       <eng-data  t="0.05" f="325." m="308.023" cg="183.5"/>\r
  16       <eng-data  t="0.07" f="275." m="305.076" cg="183.5"/>\r
  17       <eng-data  t="0.14" f="292." m="295.327" cg="183.5"/>\r
  18       <eng-data  t="0.26" f="296." m="277.995" cg="183.5"/>\r
  19       <eng-data  t="0.8" f="280." m="201.593" cg="183.5"/>\r
  20       <eng-data  t="1.1" f="280.4" m="160.298" cg="183.5"/>\r
  21       <eng-data  t="1.62" f="255." m="91.9118" cg="183.5"/>\r
  22       <eng-data  t="1.8" f="226." m="70.645" cg="183.5"/>\r
  23       <eng-data  t="2.105" f="210." m="37.9809" cg="183.5"/>\r
  24       <eng-data  t="2.2" f="195." m="28.5302" cg="183.5"/>\r
  25       <eng-data  t="2.45" f="80." m="11.643" cg="183.5"/>\r
  26       <eng-data  t="2.75" f="36." m="3.09496" cg="183.5"/>\r
  27       <eng-data  t="3.1" f="0." m="0." cg="183.5"/>\r
  28     </data>\r
  29   </engine>\r
  30 </engine-list>\r
  31 </engine-database>\r