git.gag.com Git - debian/openrocket/blob - datafiles/thrustcurves/AeroTech_F12.rse

   1 <engine-database>\r
   2  <engine-list>\r
   3 <engine FDiv="10" FFix="1" FStep="-1." Isp="145.37" Itot="43.195" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="14.742" burn-time="2.93" cgDiv="10" cgFix="1" cgStep="-1." code="F12" delays="2,5" dia="24." exitDia="0." initWt="66.7" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="45.43" mfg="Aerotech" peakThrust="23.54" propWt="30.3" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
   4 <comments>Aerotech F12 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="30.3" t="0."/>\r
  14 <eng-data cg="35." f="20.894" m="30.0289" t="0.037"/>\r
  15 <eng-data cg="35." f="22.152" m="29.7722" t="0.054"/>\r
  16 <eng-data cg="35." f="22.152" m="29.0419" t="0.101"/>\r
  17 <eng-data cg="35." f="22.571" m="28.3046" t="0.148"/>\r
  18 <eng-data cg="35." f="23.409" m="28.0305" t="0.165"/>\r
  19 <eng-data cg="35." f="22.421" m="27.4679" t="0.2"/>\r
  20 <eng-data cg="35." f="22.142" m="26.2019" t="0.281"/>\r
  21 <eng-data cg="35." f="22.132" m="24.8354" t="0.369"/>\r
  22 <eng-data cg="35." f="22.271" m="23.2002" t="0.474"/>\r
  23 <eng-data cg="35." f="23.54" m="22.3647" t="0.526"/>\r
  24 <eng-data cg="35." f="21.982" m="21.9974" t="0.549"/>\r
  25 <eng-data cg="35." f="22.122" m="20.6362" t="0.637"/>\r
  26 <eng-data cg="35." f="21.842" m="19.2947" t="0.724"/>\r
  27 <eng-data cg="35." f="21.413" m="18.1417" t="0.8"/>\r
  28 <eng-data cg="35." f="22.251" m="17.7895" t="0.823"/>\r
  29 <eng-data cg="35." f="20.714" m="17.4429" t="0.846"/>\r
  30 <eng-data cg="35." f="21.553" m="16.924" t="0.881"/>\r
  31 <eng-data cg="35." f="21.123" m="15.9661" t="0.945"/>\r
  32 <eng-data cg="35." f="20.704" m="14.8511" t="1.021"/>\r
  33 <eng-data cg="35." f="20.554" m="13.5054" t="1.114"/>\r
  34 <eng-data cg="35." f="19.296" m="12.1217" t="1.213"/>\r
  35 <eng-data cg="35." f="18.298" m="9.89334" t="1.382"/>\r
  36 <eng-data cg="35." f="18.019" m="8.63232" t="1.481"/>\r
  37 <eng-data cg="35." f="15.343" m="5.63682" t="1.737"/>\r
  38 <eng-data cg="35." f="17.3" m="5.03003" t="1.79"/>\r
  39 <eng-data cg="35." f="13.936" m="4.01116" t="1.883"/>\r
  40 <eng-data cg="35." f="11.26" m="2.52654" t="2.051"/>\r
  41 <eng-data cg="35." f="7.468" m="1.41646" t="2.22"/>\r
  42 <eng-data cg="35." f="3.671" m="0.529609" t="2.447"/>\r
  43 <eng-data cg="35." f="1.135" m="0.0879761" t="2.709"/>\r
  44 <eng-data cg="35." f="0." m="0." t="2.93"/>\r
  45 </data>\r
  46 </engine>\r
  47  </engine-list>\r
  48 </engine-database>\r