version 1.0.0
[debian/openrocket] / datafiles / thrustcurves / AeroTech_M1297.rse
1 <engine-database>\r
2  <engine-list>\r
3 <engine FDiv="10" FFix="1" FStep="-1." Isp="203.79" Itot="5439.04" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="1304.33" burn-time="4.17" cgDiv="10" cgFix="1" cgStep="-1." code="M1297W" delays="1000" dia="75." exitDia="0." initWt="4636.8" len="665.48" mDiv="10" mFix="1" mStep="-1." massFrac="58.7" mfg="Aerotech" peakThrust="2047.83" propWt="2721.6" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
4 <data>\r
5 <eng-data cg="332.74" f="0." m="2721.6" t="0."/>\r
6 <eng-data cg="332.74" f="2047.83" m="2706.23" t="0.03"/>\r
7 <eng-data cg="332.74" f="1891.3" m="2656.95" t="0.08"/>\r
8 <eng-data cg="332.74" f="1734.78" m="2275.92" t="0.5"/>\r
9 <eng-data cg="332.74" f="1669.57" m="1850.05" t="1."/>\r
10 <eng-data cg="332.74" f="1650." m="1434.79" t="1.5"/>\r
11 <eng-data cg="332.74" f="1558.7" m="1033.4" t="2."/>\r
12 <eng-data cg="332.74" f="1336.96" m="671.162" t="2.5"/>\r
13 <eng-data cg="332.74" f="1115.22" m="364.405" t="3."/>\r
14 <eng-data cg="332.74" f="1069.57" m="162.157" t="3.37"/>\r
15 <eng-data cg="332.74" f="710.87" m="95.3393" t="3.52"/>\r
16 <eng-data cg="332.74" f="489.13" m="71.321" t="3.6"/>\r
17 <eng-data cg="332.74" f="182.61" m="9.13748" t="3.97"/>\r
18 <eng-data cg="332.74" f="0." m="0." t="4.17"/>\r
19 </data>\r
20 </engine>\r
21  </engine-list>\r
22 </engine-database>\r