git.gag.com Git - debian/openrocket/blob - datafiles/thrustcurves/AeroTech_M1550.rse

   1 <engine-database>\r
   2  <engine-list>\r
   3 <engine FDiv="10" FFix="1" FStep="-1." Isp="161.41" Itot="5529.12" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1531.61" burn-time="3.61" cgDiv="10" cgFix="1" cgStep="-1." code="M1550R" delays="1000" dia="75." exitDia="0." initWt="5715." len="800." mDiv="10" mFix="1" mStep="-1." massFrac="61.12" mfg="Aerotech" peakThrust="2125.33" propWt="3493." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
   4 <data>\r
   5 <eng-data cg="400." f="0." m="3493." t="0."/>\r
   6 <eng-data cg="400." f="1720.76" m="3454.95" t="0.07"/>\r
   7 <eng-data cg="400." f="2125.33" m="3284.87" t="0.21"/>\r
   8 <eng-data cg="400." f="1995.95" m="3089.6" t="0.36"/>\r
   9 <eng-data cg="400." f="1908.44" m="2916.94" t="0.5"/>\r
  10 <eng-data cg="400." f="1868.71" m="2737.97" t="0.65"/>\r
  11 <eng-data cg="400." f="1835.5" m="2574.16" t="0.79"/>\r
  12 <eng-data cg="400." f="1808.66" m="2401.5" t="0.94"/>\r
  13 <eng-data cg="400." f="1796.3" m="2242.08" t="1.08"/>\r
  14 <eng-data cg="400." f="1785.42" m="2083.69" t="1.22"/>\r
  15 <eng-data cg="400." f="1773.15" m="1915.08" t="1.37"/>\r
  16 <eng-data cg="400." f="1746.59" m="1759.43" t="1.51"/>\r
  17 <eng-data cg="400." f="1715.71" m="1595.38" t="1.66"/>\r
  18 <eng-data cg="400." f="1689.63" m="1444.79" t="1.8"/>\r
  19 <eng-data cg="400." f="1660.72" m="1286.05" t="1.95"/>\r
  20 <eng-data cg="400." f="1633.28" m="1140.38" t="2.09"/>\r
  21 <eng-data cg="400." f="1606.04" m="997.13" t="2.23"/>\r
  22 <eng-data cg="400." f="1570.22" m="846.636" t="2.38"/>\r
  23 <eng-data cg="400." f="1534.71" m="709.329" t="2.52"/>\r
  24 <eng-data cg="400." f="1503.35" m="565.382" t="2.67"/>\r
  25 <eng-data cg="400." f="1461.32" m="434.278" t="2.81"/>\r
  26 <eng-data cg="400." f="1427.57" m="297.4" t="2.96"/>\r
  27 <eng-data cg="400." f="1393.23" m="172.657" t="3.1"/>\r
  28 <eng-data cg="400." f="939.96" m="69.4785" t="3.24"/>\r
  29 <eng-data cg="400." f="268.5" m="12.2204" t="3.39"/>\r
  30 <eng-data cg="400." f="4.99" m="0.126097" t="3.53"/>\r
  31 <eng-data cg="400." f="0." m="0." t="3.61"/>\r
  32 </data>\r
  33 </engine>\r
  34  </engine-list>\r
  35 </engine-database>\r