version 1.0.0
[debian/openrocket] / datafiles / thrustcurves / AeroTech_I284.rse
1 <engine-database>\r
2  <engine-list>\r
3 <engine FDiv="10" FFix="1" FStep="-1." Isp="180.85" Itot="554.236" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="307.909" burn-time="1.8" cgDiv="10" cgFix="1" cgStep="-1." code="I284W" delays="6,10,14" dia="38." exitDia="0." initWt="567.8" len="297." mDiv="10" mFix="1" mStep="-1." massFrac="55.04" mfg="Aerotech" peakThrust="487.77" propWt="312.5" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
4 <data>\r
5 <eng-data cg="148.5" f="0." m="312.5" t="0."/>\r
6 <eng-data cg="148.5" f="487.77" m="312.5" t="0."/>\r
7 <eng-data cg="148.5" f="408.77" m="287.225" t="0.1"/>\r
8 <eng-data cg="148.5" f="408.77" m="264.177" t="0.2"/>\r
9 <eng-data cg="148.5" f="430.74" m="216.842" t="0.4"/>\r
10 <eng-data cg="148.5" f="413.18" m="169.258" t="0.6"/>\r
11 <eng-data cg="148.5" f="307.67" m="67.6475" t="1.1"/>\r
12 <eng-data cg="148.5" f="250.51" m="36.1751" t="1.3"/>\r
13 <eng-data cg="148.5" f="193.35" m="11.1485" t="1.5"/>\r
14 <eng-data cg="148.5" f="79.08" m="3.46818" t="1.6"/>\r
15 <eng-data cg="148.5" f="21.97" m="0.619377" t="1.7"/>\r
16 <eng-data cg="148.5" f="0." m="0." t="1.8"/>\r
17 </data>\r
18 </engine>\r
19  </engine-list>\r
20 </engine-database>\r