git.gag.com Git - debian/openrocket/blob - datafiles/thrustcurves/Apogee_E6.rse

   1 <engine-database>\r
   2  <engine-list>\r
   3 <engine FDiv="10" FFix="1" FStep="-1." Isp="183.39" Itot="38.667" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="6.381" burn-time="6.06" cgDiv="10" cgFix="1" cgStep="-1." code="E6" delays="2,4,6,8,100" dia="24." exitDia="0." initWt="46.3" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="46.44" mfg="Apogee" peakThrust="20.12" propWt="21.5" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
   4 <comments>Aerotech E6 RASP.ENG file made from NAR published data\r
   5 File produced July 4, 2000\r
   6 The total impulse, peak thrust, average thrust and burn time are\r
   7 the same as the averaged static test data on the NAR web site in\r
   8 the certification file. The curve drawn with these data points is as\r
   9 close to the certification curve as can be with such a limited\r
  10 number of points (32) allowed with wRASP up to v1.6.\r
  11 </comments>\r
  12 <data>\r
  13 <eng-data cg="35." f="0." m="21.5" t="0."/>\r
  14 <eng-data cg="35." f="18.59" m="21.2106" t="0.056"/>\r
  15 <eng-data cg="35." f="20.12" m="20.6079" t="0.112"/>\r
  16 <eng-data cg="35." f="17.575" m="20.021" t="0.168"/>\r
  17 <eng-data cg="35." f="14.38" m="18.7862" t="0.307"/>\r
  18 <eng-data cg="35." f="10.45" m="17.2399" t="0.531"/>\r
  19 <eng-data cg="35." f="7.696" m="15.4086" t="0.894"/>\r
  20 <eng-data cg="35." f="6.244" m="14.432" t="1.146"/>\r
  21 <eng-data cg="35." f="5.808" m="12.6059" t="1.691"/>\r
  22 <eng-data cg="35." f="5.663" m="8.95436" t="2.836"/>\r
  23 <eng-data cg="35." f="5.517" m="5.65345" t="3.898"/>\r
  24 <eng-data cg="35." f="5.227" m="4.52736" t="4.275"/>\r
  25 <eng-data cg="35." f="4.937" m="4.13176" t="4.415"/>\r
  26 <eng-data cg="35." f="5.082" m="2.34073" t="5.058"/>\r
  27 <eng-data cg="35." f="5.227" m="1.01948" t="5.519"/>\r
  28 <eng-data cg="35." f="6.679" m="0.741439" t="5.603"/>\r
  29 <eng-data cg="35." f="3.921" m="0.370124" t="5.729"/>\r
  30 <eng-data cg="35." f="2.323" m="0.104528" t="5.882"/>\r
  31 <eng-data cg="35." f="1.016" m="0.0265515" t="5.966"/>\r
  32 <eng-data cg="35." f="0." m="-0." t="6.06"/>\r
  33 </data>\r
  34 </engine>\r
  35  </engine-list>\r
  36 </engine-database>\r