version 1.0.0
[debian/openrocket] / datafiles / thrustcurves / Estes_B6.rse
1 <engine-database>\r
2  <engine-list>\r
3 <engine FDiv="10" FFix="1" FStep="-1." Isp="78.81" Itot="4.328" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="5.033" burn-time="0.86" cgDiv="10" cgFix="1" cgStep="-1." code="B6" delays="0,2,4,6" dia="18." exitDia="0." initWt="18.22" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="30.74" mfg="Estes" peakThrust="12.14" propWt="5.6" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
4 <comments>Estes B6 RASP.ENG file made from NAR published data\r
5 File produced October 3, 2000\r
6 The total impulse, peak thrust, average thrust and burn time are\r
7 the same as the averaged static test data on the NAR web site in\r
8 the certification file. The curve drawn with these data points is as\r
9 close to the certification curve as can be with such a limited\r
10 number of points (32) allowed with wRASP up to v1.6.\r
11 </comments>\r
12 <data>\r
13 <eng-data cg="35." f="0." m="5.6" t="0."/>\r
14 <eng-data cg="35." f="0.688" m="5.58976" t="0.023"/>\r
15 <eng-data cg="35." f="2.457" m="5.52059" t="0.057"/>\r
16 <eng-data cg="35." f="4.816" m="5.37002" t="0.089"/>\r
17 <eng-data cg="35." f="7.274" m="5.15884" t="0.116"/>\r
18 <eng-data cg="35." f="9.929" m="4.80271" t="0.148"/>\r
19 <eng-data cg="35." f="12.14" m="4.47433" t="0.171"/>\r
20 <eng-data cg="35." f="11.695" m="4.16594" t="0.191"/>\r
21 <eng-data cg="35." f="10.719" m="4.03544" t="0.2"/>\r
22 <eng-data cg="35." f="9.24" m="3.91923" t="0.209"/>\r
23 <eng-data cg="35." f="7.667" m="3.68954" t="0.23"/>\r
24 <eng-data cg="35." f="6.488" m="3.4606" t="0.255"/>\r
25 <eng-data cg="35." f="5.505" m="3.07267" t="0.305"/>\r
26 <eng-data cg="35." f="4.816" m="2.60528" t="0.375"/>\r
27 <eng-data cg="35." f="4.62" m="1.98262" t="0.477"/>\r
28 <eng-data cg="35." f="4.62" m="1.36692" t="0.58"/>\r
29 <eng-data cg="35." f="4.521" m="0.828784" t="0.671"/>\r
30 <eng-data cg="35." f="4.226" m="0.404379" t="0.746"/>\r
31 <eng-data cg="35." f="4.325" m="0.183102" t="0.786"/>\r
32 <eng-data cg="35." f="3.145" m="0.105781" t="0.802"/>\r
33 <eng-data cg="35." f="1.572" m="0.0355943" t="0.825"/>\r
34 <eng-data cg="35." f="0." m="0." t="0.86"/>\r
35 </data>\r
36 </engine>\r
37  </engine-list>\r
38 </engine-database>\r