git.gag.com Git - debian/openrocket/blob - datafiles/thrustcurves/AeroTech_G64.rse

   1 <engine-database>\r
   2  <engine-list>\r
   3 <engine FDiv="10" FFix="1" FStep="-1." Isp="193.83" Itot="118.803" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="56.844" burn-time="2.09" cgDiv="10" cgFix="1" cgStep="-1." code="G64" delays="4,8,10" dia="29." exitDia="0." initWt="151.2" len="124." mDiv="10" mFix="1" mStep="-1." massFrac="41.34" mfg="Aerotech" peakThrust="98.31" propWt="62.5" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
   4 <comments>Aerotech G64 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="62." f="0." m="62.5" t="0."/>\r
  14 <eng-data cg="62." f="54.325" m="62.2999" t="0.014"/>\r
  15 <eng-data cg="62." f="81.488" m="61.6569" t="0.032"/>\r
  16 <eng-data cg="62." f="98.31" m="60.38" t="0.059"/>\r
  17 <eng-data cg="62." f="85.021" m="58.3546" t="0.101"/>\r
  18 <eng-data cg="62." f="83.847" m="55.5117" t="0.165"/>\r
  19 <eng-data cg="62." f="85.614" m="50.6531" t="0.274"/>\r
  20 <eng-data cg="62." f="87.39" m="46.2844" t="0.37"/>\r
  21 <eng-data cg="62." f="86.798" m="41.4276" t="0.476"/>\r
  22 <eng-data cg="62." f="91.516" m="40.1612" t="0.503"/>\r
  23 <eng-data cg="62." f="85.614" m="39.5089" t="0.517"/>\r
  24 <eng-data cg="62." f="83.847" m="36.4778" t="0.585"/>\r
  25 <eng-data cg="62." f="80.896" m="30.4977" t="0.723"/>\r
  26 <eng-data cg="62." f="82.07" m="29.5546" t="0.745"/>\r
  27 <eng-data cg="62." f="77.945" m="28.3761" t="0.773"/>\r
  28 <eng-data cg="62." f="75.576" m="23.9341" t="0.883"/>\r
  29 <eng-data cg="62." f="74.401" m="19.7918" t="0.988"/>\r
  30 <eng-data cg="62." f="69.673" m="15.8126" t="1.093"/>\r
  31 <eng-data cg="62." f="61.412" m="9.98534" t="1.262"/>\r
  32 <eng-data cg="62." f="61.994" m="9.40105" t="1.28"/>\r
  33 <eng-data cg="62." f="58.451" m="7.94368" t="1.326"/>\r
  34 <eng-data cg="62." f="54.907" m="6.57206" t="1.372"/>\r
  35 <eng-data cg="62." f="47.238" m="5.22865" t="1.422"/>\r
  36 <eng-data cg="62." f="34.841" m="3.43667" t="1.505"/>\r
  37 <eng-data cg="62." f="23.027" m="2.12761" t="1.591"/>\r
  38 <eng-data cg="62." f="13.581" m="1.06837" t="1.701"/>\r
  39 <eng-data cg="62." f="7.085" m="0.372564" t="1.829"/>\r
  40 <eng-data cg="62." f="4.133" m="0.157156" t="1.902"/>\r
  41 <eng-data cg="62." f="1.771" m="0.0577648" t="1.966"/>\r
  42 <eng-data cg="62." f="0." m="0." t="2.09"/>\r
  43 </data>\r
  44 </engine>\r
  45  </engine-list>\r
  46 </engine-database>\r