version 1.0.0
[debian/openrocket] / datafiles / thrustcurves / AeroTech_I300.rse
1 <engine-database>\r
2  <engine-list>\r
3 <engine FDiv="10" FFix="1" FStep="-1." Isp="200.99" Itot="436.789" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="272.993" burn-time="1.6" cgDiv="10" cgFix="1" cgStep="-1." code="I300T" delays="6,10,14" dia="38." exitDia="0." initWt="440.5" len="250." mDiv="10" mFix="1" mStep="-1." massFrac="50.31" mfg="Aerotech" peakThrust="473.17" propWt="221.6" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
4 <data>\r
5 <eng-data cg="125." f="0." m="221.6" t="0."/>\r
6 <eng-data cg="125." f="473.17" m="221.6" t="0."/>\r
7 <eng-data cg="125." f="395.68" m="199.56" t="0.1"/>\r
8 <eng-data cg="125." f="375.31" m="180.002" t="0.2"/>\r
9 <eng-data cg="125." f="367.14" m="161.169" t="0.3"/>\r
10 <eng-data cg="125." f="358.97" m="142.749" t="0.4"/>\r
11 <eng-data cg="125." f="346.72" m="124.848" t="0.5"/>\r
12 <eng-data cg="125." f="338.56" m="107.465" t="0.6"/>\r
13 <eng-data cg="125." f="318.19" m="90.8051" t="0.7"/>\r
14 <eng-data cg="125." f="305.94" m="74.9729" t="0.8"/>\r
15 <eng-data cg="125." f="295.35" m="59.72" t="0.9"/>\r
16 <eng-data cg="125." f="269.23" m="35.3732" t="1.07"/>\r
17 <eng-data cg="125." f="258.01" m="31.3609" t="1.1"/>\r
18 <eng-data cg="125." f="246.79" m="18.5556" t="1.2"/>\r
19 <eng-data cg="125." f="179.49" m="7.74224" t="1.3"/>\r
20 <eng-data cg="125." f="48.95" m="1.94742" t="1.4"/>\r
21 <eng-data cg="125." f="13.91" m="0.352854" t="1.5"/>\r
22 <eng-data cg="125." f="0." m="0." t="1.6"/>\r
23 </data>\r
24 </engine>\r
25  </engine-list>\r
26 </engine-database>\r