version 1.0.0
[debian/openrocket] / datafiles / thrustcurves / KBA_G135.rse
1 <engine-database>\r
2   <engine-list>\r
3   <engine  mfg="Kosdon-by-Aerotech" code="G135R" Type="reloadable" dia="29." len="206."\r
4 initWt="226." propWt="80." delays="6,10,14" auto-calc-mass="1" auto-calc-cg="1"\r
5 avgThrust="136.999" peakThrust="158.178" throatDia="0." exitDia="0."\r
6 Itot="143.712" burn-time="1.05" massFrac="35.4" Isp="183.18" tDiv="10"\r
7 tStep="-1." tFix="1" FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1."\r
8 mFix="1" cgDiv="10" cgStep="-1." cgFix="1">\r
9   <comments>Input by Tim Van Milligan for RockSim users. Used John Coker's ThrustCruve\r
10 Tracer program. Thrust curve and engine data TRA certification dated Oct 14,\r
11 2008.\r
12 </comments>\r
13   <data>\r
14     <eng-data  t="0." f="0." m="80." cg="103."/>\r
15     <eng-data  t="0.011" f="156.916" m="79.5196" cg="103."/>\r
16     <eng-data  t="0.016" f="63.461" m="79.2129" cg="103."/>\r
17     <eng-data  t="0.027" f="98.191" m="78.718" cg="103."/>\r
18     <eng-data  t="0.061" f="109.872" m="76.749" cg="103."/>\r
19     <eng-data  t="0.094" f="111.135" m="74.719" cg="103."/>\r
20     <eng-data  t="0.14" f="116.187" m="71.8085" cg="103."/>\r
21     <eng-data  t="0.197" f="127.553" m="67.9415" cg="103."/>\r
22     <eng-data  t="0.26" f="135.13" m="63.3354" cg="103."/>\r
23     <eng-data  t="0.316" f="139.235" m="59.0589" cg="103."/>\r
24     <eng-data  t="0.354" f="141.445" m="56.0902" cg="103."/>\r
25     <eng-data  t="0.408" f="147.128" m="51.7529" cg="103."/>\r
26     <eng-data  t="0.459" f="149.022" m="47.5491" cg="103."/>\r
27     <eng-data  t="0.502" f="153.443" m="43.929" cg="103."/>\r
28     <eng-data  t="0.546" f="156.6" m="40.132" cg="103."/>\r
29     <eng-data  t="0.6" f="158.178" m="35.4009" cg="103."/>\r
30     <eng-data  t="0.684" f="155.968" m="28.0561" cg="103."/>\r
31     <eng-data  t="0.743" f="152.811" m="22.9854" cg="103."/>\r
32     <eng-data  t="0.816" f="149.97" m="16.8334" cg="103."/>\r
33     <eng-data  t="0.875" f="148.075" m="11.9389" cg="103."/>\r
34     <eng-data  t="0.91" f="146.812" m="9.06622" cg="103."/>\r
35     <eng-data  t="0.963" f="151.232" m="4.66954" cg="103."/>\r
36     <eng-data  t="0.981" f="152.18" m="3.14944" cg="103."/>\r
37     <eng-data  t="0.993" f="149.022" m="2.14342" cg="103."/>\r
38     <eng-data  t="1.014" f="103.558" m="0.667078" cg="103."/>\r
39     <eng-data  t="1.02" f="61.251" m="0.391845" cg="103."/>\r
40     <eng-data  t="1.034" f="22.732" m="0.0645891" cg="103."/>\r
41     <eng-data  t="1.039" f="7.893" m="0.021969" cg="103."/>\r
42     <eng-data  t="1.049" f="0." m="0." cg="103."/>\r
43   </data>\r
44 </engine>\r
45 </engine-list>\r
46 </engine-database>\r