git.gag.com Git - debian/openrocket/blob - datafiles/thrustcurves/AeroTech_F39.rse

   1 <engine-database>\r
   2  <engine-list>\r
   3 <engine FDiv="10" FFix="1" FStep="-1." Isp="223.07" Itot="49.658" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="37.337" burn-time="1.33" cgDiv="10" cgFix="1" cgStep="-1." code="F39" delays="3,6,9" dia="24." exitDia="0." initWt="60." len="70." mDiv="10" mFix="1" mStep="-1." massFrac="37.83" mfg="Aerotech" peakThrust="59.47" propWt="22.7" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
   4 <comments>Aerotech F39 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="22.7" t="0."/>\r
  14 <eng-data cg="35." f="45.057" m="22.597" t="0.01"/>\r
  15 <eng-data cg="35." f="54.131" m="22.461" t="0.016"/>\r
  16 <eng-data cg="35." f="58.321" m="21.6899" t="0.046"/>\r
  17 <eng-data cg="35." f="59.47" m="20.8015" t="0.079"/>\r
  18 <eng-data cg="35." f="58.311" m="20.1554" t="0.103"/>\r
  19 <eng-data cg="35." f="57.253" m="19.4422" t="0.13"/>\r
  20 <eng-data cg="35." f="55.491" m="18.3599" t="0.172"/>\r
  21 <eng-data cg="35." f="53.738" m="16.7871" t="0.235"/>\r
  22 <eng-data cg="35." f="51.271" m="14.723" t="0.321"/>\r
  23 <eng-data cg="35." f="50.566" m="13.7454" t="0.363"/>\r
  24 <eng-data cg="35." f="49.509" m="13.1965" t="0.387"/>\r
  25 <eng-data cg="35." f="50.203" m="12.7179" t="0.408"/>\r
  26 <eng-data cg="35." f="48.804" m="12.3106" t="0.426"/>\r
  27 <eng-data cg="35." f="47.746" m="11.7147" t="0.453"/>\r
  28 <eng-data cg="35." f="47.041" m="11.1298" t="0.48"/>\r
  29 <eng-data cg="35." f="41.059" m="7.10253" t="0.68"/>\r
  30 <eng-data cg="35." f="39.649" m="6.43844" t="0.716"/>\r
  31 <eng-data cg="35." f="38.944" m="5.79176" t="0.752"/>\r
  32 <eng-data cg="35." f="36.487" m="4.80905" t="0.809"/>\r
  33 <eng-data cg="35." f="34.382" m="3.98296" t="0.86"/>\r
  34 <eng-data cg="35." f="33.324" m="3.47228" t="0.893"/>\r
  35 <eng-data cg="35." f="32.619" m="3.11055" t="0.917"/>\r
  36 <eng-data cg="35." f="28.752" m="1.94631" t="1."/>\r
  37 <eng-data cg="35." f="25.247" m="1.02065" t="1.075"/>\r
  38 <eng-data cg="35." f="22.095" m="0.696033" t="1.105"/>\r
  39 <eng-data cg="35." f="17.201" m="0.507421" t="1.126"/>\r
  40 <eng-data cg="35." f="13.001" m="0.383167" t="1.144"/>\r
  41 <eng-data cg="35." f="8.109" m="0.238419" t="1.174"/>\r
  42 <eng-data cg="35." f="4.606" m="0.107641" t="1.219"/>\r
  43 <eng-data cg="35." f="2.5" m="0.0394269" t="1.261"/>\r
  44 <eng-data cg="35." f="0." m="0." t="1.33"/>\r
  45 </data>\r
  46 </engine>\r
  47  </engine-list>\r
  48 </engine-database>\r