version 1.0.0
[debian/openrocket] / datafiles / thrustcurves / AeroTech_I435.rse
1 <engine-database>\r
2  <engine-list>\r
3 <engine FDiv="10" FFix="1" FStep="-1." Isp="204.83" Itot="556.41" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="397.436" burn-time="1.4" cgDiv="10" cgFix="1" cgStep="-1." code="I435T" delays="6,10,14" dia="38." exitDia="0." initWt="526.9" len="297." mDiv="10" mFix="1" mStep="-1." massFrac="52.57" mfg="Aerotech" peakThrust="780.77" propWt="277." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
4 <data>\r
5 <eng-data cg="148.5" f="0." m="277." t="0."/>\r
6 <eng-data cg="148.5" f="780.77" m="277." t="0."/>\r
7 <eng-data cg="148.5" f="628.21" m="241.928" t="0.1"/>\r
8 <eng-data cg="148.5" f="583.33" m="211.771" t="0.2"/>\r
9 <eng-data cg="148.5" f="551.92" m="183.513" t="0.3"/>\r
10 <eng-data cg="148.5" f="538.46" m="156.371" t="0.4"/>\r
11 <eng-data cg="148.5" f="529.49" m="129.788" t="0.5"/>\r
12 <eng-data cg="148.5" f="507.05" m="103.987" t="0.6"/>\r
13 <eng-data cg="148.5" f="448.72" m="80.1961" t="0.7"/>\r
14 <eng-data cg="148.5" f="403.85" m="58.9741" t="0.8"/>\r
15 <eng-data cg="148.5" f="358.97" m="39.9863" t="0.9"/>\r
16 <eng-data cg="148.5" f="314.1" m="23.2324" t="1."/>\r
17 <eng-data cg="148.5" f="197.44" m="10.4993" t="1.1"/>\r
18 <eng-data cg="148.5" f="89.74" m="3.35092" t="1.2"/>\r
19 <eng-data cg="148.5" f="22.44" m="0.55857" t="1.3"/>\r
20 <eng-data cg="148.5" f="0." m="0." t="1.4"/>\r
21 </data>\r
22 </engine>\r
23  </engine-list>\r
24 </engine-database>\r