version 1.0.0
[debian/openrocket] / datafiles / thrustcurves / AeroTech_E7.rse
1 <engine-database>\r
2  <engine-list>\r
3 <engine FDiv="10" FFix="1" FStep="-1." Isp="175.03" Itot="29.351" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="5.405" burn-time="5.43" cgDiv="10" cgFix="1" cgStep="-1." code="E7RC" delays="1000" dia="24." exitDia="0." initWt="48.4" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="35.33" mfg="Aerotech" peakThrust="11.58" propWt="17.1" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
4 <comments>Aerotech E7TRC RASP.ENG file made from NAR published data\r
5 File produced July 4, 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="17.1" t="0."/>\r
14 <eng-data cg="35." f="6.636" m="17.0265" t="0.038"/>\r
15 <eng-data cg="35." f="10.056" m="16.905" t="0.063"/>\r
16 <eng-data cg="35." f="11.019" m="16.7576" t="0.087"/>\r
17 <eng-data cg="35." f="11.42" m="16.4504" t="0.134"/>\r
18 <eng-data cg="35." f="11.58" m="15.968" t="0.206"/>\r
19 <eng-data cg="35." f="11.149" m="15.2662" t="0.312"/>\r
20 <eng-data cg="35." f="10.738" m="14.2843" t="0.466"/>\r
21 <eng-data cg="35." f="9.777" m="13.0831" t="0.667"/>\r
22 <eng-data cg="35." f="8.132" m="11.6589" t="0.94"/>\r
23 <eng-data cg="35." f="6.281" m="10.4707" t="1.223"/>\r
24 <eng-data cg="35." f="5.182" m="9.59916" t="1.484"/>\r
25 <eng-data cg="35." f="4.701" m="8.95139" t="1.709"/>\r
26 <eng-data cg="35." f="4.423" m="7.88027" t="2.112"/>\r
27 <eng-data cg="35." f="4.279" m="6.19708" t="2.776"/>\r
28 <eng-data cg="35." f="4.205" m="4.87734" t="3.31"/>\r
29 <eng-data cg="35." f="4.266" m="3.35727" t="3.926"/>\r
30 <eng-data cg="35." f="4.192" m="2.18694" t="4.401"/>\r
31 <eng-data cg="35." f="4.258" m="1.60356" t="4.638"/>\r
32 <eng-data cg="35." f="4.119" m="1.34489" t="4.744"/>\r
33 <eng-data cg="35." f="3.979" m="0.448479" t="5.124"/>\r
34 <eng-data cg="35." f="3.977" m="0.228306" t="5.219"/>\r
35 <eng-data cg="35." f="3.156" m="0.130646" t="5.266"/>\r
36 <eng-data cg="35." f="1.992" m="0.0601628" t="5.313"/>\r
37 <eng-data cg="35." f="0.965" m="0.0196776" t="5.36"/>\r
38 <eng-data cg="35." f="0." m="0." t="5.43"/>\r
39 </data>\r
40 </engine>\r
41  </engine-list>\r
42 </engine-database>\r