git.gag.com Git - debian/openrocket/blob - datafiles/thrustcurves/AeroTech_E28.rse

   1 <engine-database>\r
   2  <engine-list>\r
   3 <engine FDiv="10" FFix="1" FStep="-1." Isp="219.95" Itot="39.689" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="32.532" burn-time="1.22" cgDiv="10" cgFix="1" cgStep="-1." code="E28" delays="2,5,8" dia="24." exitDia="0." initWt="54.5" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="33.76" mfg="Aerotech" peakThrust="50.52" propWt="18.4" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
   4 <comments>Aerotech E28 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="18.4" t="0."/>\r
  14 <eng-data cg="35." f="29.862" m="18.3308" t="0.01"/>\r
  15 <eng-data cg="35." f="45.139" m="18.1917" t="0.018"/>\r
  16 <eng-data cg="35." f="47.562" m="17.7619" t="0.038"/>\r
  17 <eng-data cg="35." f="50.52" m="16.7843" t="0.081"/>\r
  18 <eng-data cg="35." f="48.953" m="16.2078" t="0.106"/>\r
  19 <eng-data cg="35." f="48.263" m="15.3064" t="0.146"/>\r
  20 <eng-data cg="35." f="48.953" m="14.9684" t="0.161"/>\r
  21 <eng-data cg="35." f="48.953" m="14.1514" t="0.197"/>\r
  22 <eng-data cg="35." f="47.562" m="13.1447" t="0.242"/>\r
  23 <eng-data cg="35." f="46.18" m="11.6018" t="0.313"/>\r
  24 <eng-data cg="35." f="43.057" m="9.57468" t="0.411"/>\r
  25 <eng-data cg="35." f="40.624" m="7.96469" t="0.494"/>\r
  26 <eng-data cg="35." f="39.583" m="7.35115" t="0.527"/>\r
  27 <eng-data cg="35." f="40.274" m="7.07349" t="0.542"/>\r
  28 <eng-data cg="35." f="38.542" m="6.70809" t="0.562"/>\r
  29 <eng-data cg="35." f="36.46" m="5.47371" t="0.633"/>\r
  30 <eng-data cg="35." f="34.377" m="4.6527" t="0.683"/>\r
  31 <eng-data cg="35." f="31.244" m="3.74004" t="0.743"/>\r
  32 <eng-data cg="35." f="29.162" m="2.95591" t="0.799"/>\r
  33 <eng-data cg="35." f="26.038" m="1.95786" t="0.877"/>\r
  34 <eng-data cg="35." f="20.832" m="0.947455" t="0.97"/>\r
  35 <eng-data cg="35." f="17.359" m="0.628755" t="1.006"/>\r
  36 <eng-data cg="35." f="11.462" m="0.361524" t="1.046"/>\r
  37 <eng-data cg="35." f="6.943" m="0.178072" t="1.089"/>\r
  38 <eng-data cg="35." f="3.819" m="0.0708017" t="1.132"/>\r
  39 <eng-data cg="35." f="1.735" m="0.0193045" t="1.172"/>\r
  40 <eng-data cg="35." f="0." m="0." t="1.22"/>\r
  41 </data>\r
  42 </engine>\r
  43  </engine-list>\r
  44 </engine-database>\r