git.gag.com Git - debian/openrocket/blob - core/resources/datafiles/thrustcurves/AeroTech_F32_1.rse

   1 <engine-database>\r
   2  <engine-list>\r
   3 <engine FDiv="10" FFix="1" FStep="-1." Isp="214.23" Itot="79.202" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="29.118" burn-time="2.72" cgDiv="10" cgFix="1" cgStep="-1." code="F32" delays="5,10,15" dia="24." exitDia="0." initWt="81.4" len="124." mDiv="10" mFix="1" mStep="-1." massFrac="46.31" mfg="Aerotech" peakThrust="55.64" propWt="37.7" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
   4 <comments>Aerotech F32 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="37.7" t="0."/>\r
  14 <eng-data cg="62." f="46.699" m="37.4221" t="0.025"/>\r
  15 <eng-data cg="62." f="51.846" m="37.2814" t="0.031"/>\r
  16 <eng-data cg="62." f="55.64" m="36.514" t="0.061"/>\r
  17 <eng-data cg="62." f="52.868" m="35.8942" t="0.085"/>\r
  18 <eng-data cg="62." f="47.37" m="34.9161" t="0.126"/>\r
  19 <eng-data cg="62." f="45.637" m="32.2819" t="0.245"/>\r
  20 <eng-data cg="62." f="44.946" m="30.2339" t="0.34"/>\r
  21 <eng-data cg="62." f="42.873" m="29.1052" t="0.394"/>\r
  22 <eng-data cg="62." f="42.873" m="28.0236" t="0.447"/>\r
  23 <eng-data cg="62." f="41.14" m="25.5243" t="0.572"/>\r
  24 <eng-data cg="62." f="39.408" m="22.6871" t="0.72"/>\r
  25 <eng-data cg="62." f="40.78" m="22.229" t="0.744"/>\r
  26 <eng-data cg="62." f="38.026" m="21.4413" t="0.786"/>\r
  27 <eng-data cg="62." f="35.592" m="16.9735" t="1.041"/>\r
  28 <eng-data cg="62." f="33.179" m="15.4186" t="1.136"/>\r
  29 <eng-data cg="62." f="34.541" m="14.7578" t="1.177"/>\r
  30 <eng-data cg="62." f="32.818" m="13.9882" t="1.225"/>\r
  31 <eng-data cg="62." f="31.436" m="11.6332" t="1.379"/>\r
  32 <eng-data cg="62." f="30.394" m="10.2353" t="1.474"/>\r
  33 <eng-data cg="62." f="28.311" m="7.98582" t="1.635"/>\r
  34 <eng-data cg="62." f="27.28" m="7.44337" t="1.676"/>\r
  35 <eng-data cg="62." f="29.683" m="7.19934" t="1.694"/>\r
  36 <eng-data cg="62." f="26.929" m="6.95681" t="1.712"/>\r
  37 <eng-data cg="62." f="25.537" m="5.18369" t="1.854"/>\r
  38 <eng-data cg="62." f="23.815" m="4.13832" t="1.943"/>\r
  39 <eng-data cg="62." f="21.051" m="2.54729" t="2.092"/>\r
  40 <eng-data cg="62." f="18.287" m="1.65787" t="2.187"/>\r
  41 <eng-data cg="62." f="13.82" m="0.977781" t="2.276"/>\r
  42 <eng-data cg="62." f="7.281" m="0.445449" t="2.382"/>\r
  43 <eng-data cg="62." f="2.457" m="0.114029" t="2.525"/>\r
  44 <eng-data cg="62." f="0." m="0." t="2.72"/>\r
  45 </data>\r
  46 </engine>\r
  47  </engine-list>\r
  48 </engine-database>\r