git.gag.com Git - debian/openrocket/blob - datafiles/thrustcurves/AeroTech_K695.rse

   1 <engine-database>\r
   2  <engine-list>\r
   3 <engine FDiv="10" FFix="1" FStep="-1." Isp="163.91" Itot="1496.47" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="665.099" burn-time="2.25" cgDiv="10" cgFix="1" cgStep="-1." code="K695R" delays="10,14,1000" dia="54." exitDia="0." initWt="1506." len="410." mDiv="10" mFix="1" mStep="-1." massFrac="61.82" mfg="Aerotech" peakThrust="900.13" propWt="931." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
   4 <data>\r
   5 <eng-data cg="205." f="0." m="931." t="0."/>\r
   6 <eng-data cg="205." f="618.61" m="923.303" t="0.04"/>\r
   7 <eng-data cg="205." f="727.84" m="885.608" t="0.13"/>\r
   8 <eng-data cg="205." f="752." m="844.179" t="0.22"/>\r
   9 <eng-data cg="205." f="812.48" m="800.38" t="0.31"/>\r
  10 <eng-data cg="205." f="900.13" m="752.434" t="0.4"/>\r
  11 <eng-data cg="205." f="884.76" m="696.912" t="0.5"/>\r
  12 <eng-data cg="205." f="873.46" m="653.158" t="0.58"/>\r
  13 <eng-data cg="205." f="864.56" m="599.095" t="0.68"/>\r
  14 <eng-data cg="205." f="849.67" m="551.104" t="0.77"/>\r
  15 <eng-data cg="205." f="838.89" m="503.831" t="0.86"/>\r
  16 <eng-data cg="205." f="822.55" m="457.318" t="0.95"/>\r
  17 <eng-data cg="205." f="806.24" m="411.718" t="1.04"/>\r
  18 <eng-data cg="205." f="781.34" m="367.273" t="1.13"/>\r
  19 <eng-data cg="205." f="753.97" m="324.29" t="1.22"/>\r
  20 <eng-data cg="205." f="728.47" m="282.788" t="1.31"/>\r
  21 <eng-data cg="205." f="697.63" m="242.863" t="1.4"/>\r
  22 <eng-data cg="205." f="672.98" m="204.492" t="1.49"/>\r
  23 <eng-data cg="205." f="646.66" m="167.548" t="1.58"/>\r
  24 <eng-data cg="205." f="620.9" m="132.061" t="1.67"/>\r
  25 <eng-data cg="205." f="595.57" m="98.0051" t="1.76"/>\r
  26 <eng-data cg="205." f="571.72" m="65.3259" t="1.85"/>\r
  27 <eng-data cg="205." f="546.82" m="34.0114" t="1.94"/>\r
  28 <eng-data cg="205." f="272.82" m="11.0649" t="2.03"/>\r
  29 <eng-data cg="205." f="57.95" m="1.80474" t="2.12"/>\r
  30 <eng-data cg="205." f="4.51" m="0.0561161" t="2.21"/>\r
  31 <eng-data cg="205." f="0." m="0." t="2.25"/>\r
  32 </data>\r
  33 </engine>\r
  34  </engine-list>\r
  35 </engine-database>\r