git.gag.com Git - debian/openrocket/blob - datafiles/thrustcurves/AeroTech_F22.rse

   1 <engine-database>\r
   2  <engine-list>\r
   3 <engine FDiv="10" FFix="1" FStep="-1." Isp="143.15" Itot="64.997" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="19.637" burn-time="3.31" cgDiv="10" cgFix="1" cgStep="-1." code="F22" delays="4,7" dia="29." exitDia="0." initWt="134.2" len="125." mDiv="10" mFix="1" mStep="-1." massFrac="34.5" mfg="Aerotech" peakThrust="31.15" propWt="46.3" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
   4 <comments>Aerotech F22 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="62.5" f="0." m="46.3" t="0."/>\r
  14 <eng-data cg="62.5" f="11.527" m="46.2425" t="0.014"/>\r
  15 <eng-data cg="62.5" f="20.126" m="45.5548" t="0.075"/>\r
  16 <eng-data cg="62.5" f="26.572" m="44.191" t="0.157"/>\r
  17 <eng-data cg="62.5" f="29.113" m="41.4936" t="0.293"/>\r
  18 <eng-data cg="62.5" f="30.278" m="39.611" t="0.382"/>\r
  19 <eng-data cg="62.5" f="29.69" m="38.1586" t="0.45"/>\r
  20 <eng-data cg="62.5" f="30.667" m="36.2453" t="0.539"/>\r
  21 <eng-data cg="62.5" f="30.089" m="34.6223" t="0.614"/>\r
  22 <eng-data cg="62.5" f="31.15" m="33.5754" t="0.662"/>\r
  23 <eng-data cg="62.5" f="30.478" m="31.1828" t="0.771"/>\r
  24 <eng-data cg="62.5" f="29.89" m="27.3771" t="0.948"/>\r
  25 <eng-data cg="62.5" f="28.714" m="26.3752" t="0.996"/>\r
  26 <eng-data cg="62.5" f="28.136" m="24.7148" t="1.078"/>\r
  27 <eng-data cg="62.5" f="27.738" m="22.5457" t="1.187"/>\r
  28 <eng-data cg="62.5" f="26.761" m="20.5658" t="1.289"/>\r
  29 <eng-data cg="62.5" f="26.96" m="19.6473" t="1.337"/>\r
  30 <eng-data cg="62.5" f="25.984" m="18.2331" t="1.412"/>\r
  31 <eng-data cg="62.5" f="25.008" m="17.107" t="1.474"/>\r
  32 <eng-data cg="62.5" f="26.173" m="16.3596" t="1.515"/>\r
  33 <eng-data cg="62.5" f="24.808" m="15.8694" t="1.542"/>\r
  34 <eng-data cg="62.5" f="22.856" m="13.0852" t="1.706"/>\r
  35 <eng-data cg="62.5" f="20.903" m="9.46934" t="1.938"/>\r
  36 <eng-data cg="62.5" f="18.173" m="7.20075" t="2.101"/>\r
  37 <eng-data cg="62.5" f="19.338" m="6.82667" t="2.129"/>\r
  38 <eng-data cg="62.5" f="16.21" m="5.28201" t="2.251"/>\r
  39 <eng-data cg="62.5" f="13.48" m="3.68523" t="2.402"/>\r
  40 <eng-data cg="62.5" f="8.791" m="1.79735" t="2.64"/>\r
  41 <eng-data cg="62.5" f="3.32" m="0.412687" t="2.961"/>\r
  42 <eng-data cg="62.5" f="0." m="0." t="3.31"/>\r
  43 </data>\r
  44 </engine>\r
  45  </engine-list>\r
  46 </engine-database>\r