version 1.0.0
[debian/openrocket] / datafiles / thrustcurves / AeroTech_K560.rse
1 <engine-database>\r
2  <engine-list>\r
3 <engine FDiv="10" FFix="1" FStep="-1." Isp="178.67" Itot="2467.2" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="496.918" burn-time="4.96" cgDiv="10" cgFix="1" cgStep="-1." code="K560W" delays="1000" dia="75." exitDia="0." initWt="2713.54" len="396." mDiv="10" mFix="1" mStep="-1." massFrac="51.89" mfg="Aerotech" peakThrust="789.305" propWt="1408.06" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
4 <data>\r
5 <eng-data cg="198." f="0." m="1408.06" t="0."/>\r
6 <eng-data cg="198." f="552.123" m="1392.94" t="0.096"/>\r
7 <eng-data cg="198." f="645.403" m="1326.64" t="0.29"/>\r
8 <eng-data cg="198." f="681.109" m="1253.21" t="0.484"/>\r
9 <eng-data cg="198." f="716.167" m="1175.46" t="0.679"/>\r
10 <eng-data cg="198." f="742.678" m="1094.28" t="0.874"/>\r
11 <eng-data cg="198." f="764.778" m="1010.4" t="1.069"/>\r
12 <eng-data cg="198." f="775.71" m="924.678" t="1.264"/>\r
13 <eng-data cg="198." f="785.859" m="838.231" t="1.458"/>\r
14 <eng-data cg="198." f="789.305" m="750.582" t="1.653"/>\r
15 <eng-data cg="198." f="789.077" m="662.754" t="1.848"/>\r
16 <eng-data cg="198." f="744.622" m="577.412" t="2.043"/>\r
17 <eng-data cg="198." f="676.886" m="498.718" t="2.237"/>\r
18 <eng-data cg="198." f="614.711" m="426.848" t="2.432"/>\r
19 <eng-data cg="198." f="557.908" m="361.598" t="2.627"/>\r
20 <eng-data cg="198." f="503.641" m="302.529" t="2.822"/>\r
21 <eng-data cg="198." f="455.504" m="249.158" t="3.017"/>\r
22 <eng-data cg="198." f="412.045" m="201.131" t="3.211"/>\r
23 <eng-data cg="198." f="372.963" m="157.45" t="3.406"/>\r
24 <eng-data cg="198." f="335.987" m="118.001" t="3.601"/>\r
25 <eng-data cg="198." f="307.346" m="82.2028" t="3.796"/>\r
26 <eng-data cg="198." f="279.856" m="49.5283" t="3.991"/>\r
27 <eng-data cg="198." f="223.491" m="21.6634" t="4.185"/>\r
28 <eng-data cg="198." f="70.441" m="5.30776" t="4.38"/>\r
29 <eng-data cg="198." f="10.028" m="0.830104" t="4.575"/>\r
30 <eng-data cg="198." f="2.445" m="0.136051" t="4.77"/>\r
31 <eng-data cg="198." f="0." m="0." t="4.965"/>\r
32 </data>\r
33 </engine>\r
34  </engine-list>\r
35 </engine-database>\r