version 1.0.0
[debian/openrocket] / datafiles / thrustcurves / AeroTech_J260.rse
1 <engine-database>\r
2  <engine-list>\r
3 <engine FDiv="10" FFix="1" FStep="-1." Isp="213.85" Itot="1170.22" Type="hybrid" auto-calc-cg="1" auto-calc-mass="1" avgThrust="260.049" burn-time="4.5" cgDiv="10" cgFix="1" cgStep="-1." code="J260HW" delays="1000" dia="54." exitDia="0." initWt="1574." len="708.66" mDiv="10" mFix="1" mStep="-1." massFrac="35.45" mfg="Aerotech" peakThrust="598.969" propWt="558." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
4 <data>\r
5 <eng-data cg="354.33" f="0." m="558." t="0."/>\r
6 <eng-data cg="354.33" f="598.969" m="556.896" t="0.00772798"/>\r
7 <eng-data cg="354.33" f="475.651" m="548.977" t="0.0386399"/>\r
8 <eng-data cg="354.33" f="506.481" m="532.69" t="0.108192"/>\r
9 <eng-data cg="354.33" f="493.268" m="447.958" t="0.463679"/>\r
10 <eng-data cg="354.33" f="475.651" m="374.764" t="0.780526"/>\r
11 <eng-data cg="354.33" f="427.205" m="324.861" t="1.01236"/>\r
12 <eng-data cg="354.33" f="330.314" m="146.208" t="2.00155"/>\r
13 <eng-data cg="354.33" f="193.784" m="85.373" t="2.48841"/>\r
14 <eng-data cg="354.33" f="114.509" m="48.4514" t="2.99073"/>\r
15 <eng-data cg="354.33" f="57.2543" m="6.67749" t="4.01082"/>\r
16 <eng-data cg="354.33" f="0." m="0." t="4.5"/>\r
17 </data>\r
18 </engine>\r
19  </engine-list>\r
20 </engine-database>\r