git.gag.com Git - debian/openrocket/blob - datafiles/thrustcurves/AeroTech_D9.rse

   1 <engine-database>\r
   2  <engine-list>\r
   3 <engine FDiv="10" FFix="1" FStep="-1." Isp="189.41" Itot="18.76" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="9.979" burn-time="1.88" cgDiv="10" cgFix="1" cgStep="-1." code="D9" delays="4,7" dia="24." exitDia="0." initWt="47.1" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="21.44" mfg="Aerotech" peakThrust="20." propWt="10.1" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
   4     <comments>Aerotech D9 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="10.1" t="0."/>\r
  14       <eng-data cg="35." f="2.204" m="10.0864" t="0.023"/>\r
  15       <eng-data cg="35." f="1.653" m="10.0303" t="0.077"/>\r
  16       <eng-data cg="35." f="4.96" m="9.85228" t="0.177"/>\r
  17       <eng-data cg="35." f="8.817" m="9.51109" t="0.269"/>\r
  18       <eng-data cg="35." f="9.92" m="9.31438" t="0.308"/>\r
  19       <eng-data cg="35." f="9.368" m="9.27804" t="0.315"/>\r
  20       <eng-data cg="35." f="10.604" m="9.04686" t="0.358"/>\r
  21       <eng-data cg="35." f="11.94" m="8.70096" t="0.415"/>\r
  22       <eng-data cg="35." f="13.917" m="8.00492" t="0.515"/>\r
  23       <eng-data cg="35." f="16.675" m="7.11555" t="0.623"/>\r
  24       <eng-data cg="35." f="19.155" m="6.0739" t="0.731"/>\r
  25       <eng-data cg="35." f="20." m="5.43096" t="0.792"/>\r
  26       <eng-data cg="35." f="19.155" m="4.66154" t="0.865"/>\r
  27       <eng-data cg="35." f="19.562" m="4.41141" t="0.889"/>\r
  28       <eng-data cg="35." f="18.6" m="4.06214" t="0.923"/>\r
  29       <eng-data cg="35." f="16.12" m="2.98733" t="1.038"/>\r
  30       <eng-data cg="35." f="14.195" m="2.35899" t="1.115"/>\r
  31       <eng-data cg="35." f="12.538" m="1.85526" t="1.185"/>\r
  32       <eng-data cg="35." f="10.336" m="1.28878" t="1.277"/>\r
  33       <eng-data cg="35." f="7.44" m="0.829414" t="1.373"/>\r
  34       <eng-data cg="35." f="4.822" m="0.459729" t="1.485"/>\r
  35       <eng-data cg="35." f="2.755" m="0.200697" t="1.612"/>\r
  36       <eng-data cg="35." f="1.24" m="0.0393873" t="1.762"/>\r
  37       <eng-data cg="35." f="0." m="0." t="1.88"/>\r
  38     </data>\r
  39   </engine>\r
  40  </engine-list>\r
  41 </engine-database>\r