git.gag.com Git - debian/openrocket/blob - datafiles/thrustcurves/AeroTech_F52.rse

   1 <engine-database>\r
   2  <engine-list>\r
   3 <engine FDiv="10" FFix="1" FStep="-1." Isp="203.25" Itot="72.95" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="51.374" burn-time="1.42" cgDiv="10" cgFix="1" cgStep="-1." code="F52" delays="5,8,11" dia="29." exitDia="0." initWt="121.4" len="124." mDiv="10" mFix="1" mStep="-1." massFrac="30.15" mfg="Aerotech" peakThrust="78.95" propWt="36.6" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
   4 <comments>Aerotech F52 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="36.6" t="0."/>\r
  14 <eng-data cg="62." f="46.899" m="36.4588" t="0.012"/>\r
  15 <eng-data cg="62." f="61.778" m="35.8863" t="0.033"/>\r
  16 <eng-data cg="62." f="69.441" m="35.1292" t="0.056"/>\r
  17 <eng-data cg="62." f="73.483" m="33.6592" t="0.097"/>\r
  18 <eng-data cg="62." f="76.636" m="32.9814" t="0.115"/>\r
  19 <eng-data cg="62." f="74.381" m="32.4131" t="0.13"/>\r
  20 <eng-data cg="62." f="74.82" m="31.5523" t="0.153"/>\r
  21 <eng-data cg="62." f="78.422" m="30.9757" t="0.168"/>\r
  22 <eng-data cg="62." f="78.95" m="30.423" t="0.182"/>\r
  23 <eng-data cg="62." f="77.963" m="29.4783" t="0.206"/>\r
  24 <eng-data cg="62." f="77.504" m="28.2303" t="0.238"/>\r
  25 <eng-data cg="62." f="73.892" m="27.4707" t="0.258"/>\r
  26 <eng-data cg="62." f="72.974" m="25.4076" t="0.314"/>\r
  27 <eng-data cg="62." f="72.046" m="22.6428" t="0.39"/>\r
  28 <eng-data cg="62." f="70.679" m="21.2822" t="0.428"/>\r
  29 <eng-data cg="62." f="65.699" m="18.7848" t="0.501"/>\r
  30 <eng-data cg="62." f="62.975" m="16.719" t="0.565"/>\r
  31 <eng-data cg="62." f="58.874" m="12.9593" t="0.688"/>\r
  32 <eng-data cg="62." f="56.15" m="11.1992" t="0.749"/>\r
  33 <eng-data cg="62." f="52.517" m="8.80035" t="0.837"/>\r
  34 <eng-data cg="62." f="49.793" m="7.15779" t="0.901"/>\r
  35 <eng-data cg="62." f="46.161" m="5.47285" t="0.971"/>\r
  36 <eng-data cg="62." f="39.365" m="2.96266" t="1.088"/>\r
  37 <eng-data cg="62." f="34.386" m="1.92661" t="1.144"/>\r
  38 <eng-data cg="62." f="29.417" m="1.46246" t="1.173"/>\r
  39 <eng-data cg="62." f="20.376" m="0.850406" t="1.222"/>\r
  40 <eng-data cg="62." f="13.151" m="0.404654" t="1.275"/>\r
  41 <eng-data cg="62." f="5.461" m="0.105843" t="1.339"/>\r
  42 <eng-data cg="62." f="1.838" m="0.0142932" t="1.389"/>\r
  43 <eng-data cg="62." f="0." m="0." t="1.42"/>\r
  44 </data>\r
  45 </engine>\r
  46  </engine-list>\r
  47 </engine-database>\r