git.gag.com Git - debian/openrocket/blob - datafiles/thrustcurves/AeroTech_I600.rse

   1 <engine-database>\r
   2  <engine-list>\r
   3 <engine FDiv="10" FFix="1" FStep="-1." Isp="201.66" Itot="640.142" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="542.493" burn-time="1.18" cgDiv="10" cgFix="1" cgStep="-1." code="I600R" delays="10" dia="38." exitDia="0." initWt="617." len="344.68" mDiv="10" mFix="1" mStep="-1." massFrac="52.46" mfg="Aerotech" peakThrust="817.754" propWt="323.7" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
   4 <comments>I600R Data Entered by Tim Van Milligan\r
   5 For RockSim: www.RockSim.com\r
   6 Based on Aerotech's Reload Kit Instruction Sheet.\r
   7 Not Officially Approved by TRA or Aerotech\r
   8 </comments>\r
   9 <data>\r
  10 <eng-data cg="172.34" f="0." m="323.7" t="0."/>\r
  11 <eng-data cg="172.34" f="40.438" m="323.649" t="0.005"/>\r
  12 <eng-data cg="172.34" f="817.754" m="314.753" t="0.046"/>\r
  13 <eng-data cg="172.34" f="813.261" m="309.392" t="0.059"/>\r
  14 <eng-data cg="172.34" f="772.822" m="292.95" t="0.1"/>\r
  15 <eng-data cg="172.34" f="736.877" m="254.78" t="0.2"/>\r
  16 <eng-data cg="172.34" f="696.439" m="182.301" t="0.4"/>\r
  17 <eng-data cg="172.34" f="669.48" m="147.766" t="0.5"/>\r
  18 <eng-data cg="172.34" f="620.055" m="115.162" t="0.6"/>\r
  19 <eng-data cg="172.34" f="539.178" m="57.7157" t="0.796"/>\r
  20 <eng-data cg="172.34" f="485.261" m="32.3324" t="0.894"/>\r
  21 <eng-data cg="172.34" f="453.809" m="18.7989" t="0.951"/>\r
  22 <eng-data cg="172.34" f="435.836" m="15.8748" t="0.964"/>\r
  23 <eng-data cg="172.34" f="274.082" m="9.4131" t="1."/>\r
  24 <eng-data cg="172.34" f="152.767" m="3.80114" t="1.052"/>\r
  25 <eng-data cg="172.34" f="62.904" m="0.856571" t="1.106"/>\r
  26 <eng-data cg="172.34" f="13.48" m="0.122696" t="1.144"/>\r
  27 <eng-data cg="172.34" f="0." m="0." t="1.18"/>\r
  28 </data>\r
  29 </engine>\r
  30  </engine-list>\r
  31 </engine-database>\r