version 1.0.0
[debian/openrocket] / datafiles / thrustcurves / AeroTech_J275.rse
1 <engine-database>\r
2  <engine-list>\r
3 <engine FDiv="10" FFix="1" FStep="-1." Isp="189.65" Itot="818.693" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="255.842" burn-time="3.2" cgDiv="10" cgFix="1" cgStep="-1." code="J275W" delays="6,10,14,18" dia="54." exitDia="0." initWt="882.9" len="241." mDiv="10" mFix="1" mStep="-1." massFrac="49.86" mfg="Aerotech" peakThrust="350.5" propWt="440.2" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
4 <data>\r
5 <eng-data cg="120.5" f="0." m="440.2" t="0."/>\r
6 <eng-data cg="120.5" f="0.45" m="440.2" t="0."/>\r
7 <eng-data cg="120.5" f="331.55" m="431.274" t="0.1"/>\r
8 <eng-data cg="120.5" f="293.61" m="414.467" t="0.2"/>\r
9 <eng-data cg="120.5" f="326.8" m="331.071" t="0.7"/>\r
10 <eng-data cg="120.5" f="350.5" m="221.818" t="1.3"/>\r
11 <eng-data cg="120.5" f="350.5" m="165.281" t="1.6"/>\r
12 <eng-data cg="120.5" f="307.85" m="76.7843" t="2.1"/>\r
13 <eng-data cg="120.5" f="269.99" m="45.7146" t="2.3"/>\r
14 <eng-data cg="120.5" f="227.34" m="32.3442" t="2.4"/>\r
15 <eng-data cg="120.5" f="85.27" m="7.13133" t="2.7"/>\r
16 <eng-data cg="120.5" f="47.37" m="3.5654" t="2.8"/>\r
17 <eng-data cg="120.5" f="9.47" m="0.509189" t="3."/>\r
18 <eng-data cg="120.5" f="0." m="0." t="3.2"/>\r
19 </data>\r
20 </engine>\r
21  </engine-list>\r
22 </engine-database>\r