git.gag.com Git - debian/openrocket/blob - datafiles/thrustcurves/AeroTech_H112.rse

   1 <engine-database>\r
   2  <engine-list>\r
   3 <engine FDiv="10" FFix="1" FStep="-1." Isp="152.65" Itot="280.685" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="82.554" burn-time="3.4" cgDiv="10" cgFix="1" cgStep="-1." code="H112J" delays="6,10,14" dia="38." exitDia="0." initWt="384.8" len="191." mDiv="10" mFix="1" mStep="-1." massFrac="48.73" mfg="Aerotech" peakThrust="126.62" propWt="187.5" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
   4 <comments>Data Entered by Tim Van Milligan\r
   5 For RockSim Users. http://www.rocksim.com\r
   6 Based on Aerotech's RMS 38/240-360 Black Jack Instr. Sheet\r
   7 </comments>\r
   8 <data>\r
   9 <eng-data cg="95.5" f="0." m="187.5" t="0."/>\r
  10 <eng-data cg="95.5" f="120.014" m="180.665" t="0.1705"/>\r
  11 <eng-data cg="95.5" f="126.62" m="178.235" t="0.2"/>\r
  12 <eng-data cg="95.5" f="109.003" m="176.347" t="0.224"/>\r
  13 <eng-data cg="95.5" f="106.801" m="172.454" t="0.278"/>\r
  14 <eng-data cg="95.5" f="107.902" m="165.283" t="0.378"/>\r
  15 <eng-data cg="95.5" f="113.408" m="156.117" t="0.502"/>\r
  16 <eng-data cg="95.5" f="103.498" m="120.328" t="0.996"/>\r
  17 <eng-data cg="95.5" f="103.498" m="85.552" t="1.499"/>\r
  18 <eng-data cg="95.5" f="96.892" m="70.0239" t="1.731"/>\r
  19 <eng-data cg="95.5" f="92.487" m="51.9335" t="2.017"/>\r
  20 <eng-data cg="95.5" f="73.77" m="25.3343" t="2.496"/>\r
  21 <eng-data cg="95.5" f="42.94" m="5.76554" t="2.998"/>\r
  22 <eng-data cg="95.5" f="0." m="0." t="3.4"/>\r
  23 </data>\r
  24 </engine>\r
  25  </engine-list>\r
  26 </engine-database>\r