version 1.0.0
[debian/openrocket] / datafiles / thrustcurves / AeroTech_D21.rse
1 <engine-database>\r
2  <engine-list>\r
3 <engine FDiv="10" FFix="1" FStep="-1." Isp="208.09" Itot="19.59" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="20.841" burn-time="0.94" cgDiv="10" cgFix="1" cgStep="-1." code="D21" delays="4,7" dia="18." exitDia="0." initWt="25." len="70." mDiv="10" mFix="1" mStep="-1." massFrac="38.4" mfg="Aerotech" peakThrust="32.12" propWt="9.6" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
4 <comments>Aerotech D21 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="9.6" t="0."/>\r
14 <eng-data cg="35." f="1.367" m="9.59665" t="0.01"/>\r
15 <eng-data cg="35." f="19.367" m="9.54077" t="0.021"/>\r
16 <eng-data cg="35." f="32.12" m="9.43985" t="0.029"/>\r
17 <eng-data cg="35." f="31.667" m="9.31481" t="0.037"/>\r
18 <eng-data cg="35." f="30.528" m="9.10147" t="0.051"/>\r
19 <eng-data cg="35." f="30.074" m="8.46298" t="0.094"/>\r
20 <eng-data cg="35." f="31.213" m="8.14763" t="0.115"/>\r
21 <eng-data cg="35." f="30.074" m="7.87734" t="0.133"/>\r
22 <eng-data cg="35." f="30.76" m="7.2215" t="0.177"/>\r
23 <eng-data cg="35." f="29.842" m="7.04331" t="0.189"/>\r
24 <eng-data cg="35." f="30.528" m="6.83623" t="0.203"/>\r
25 <eng-data cg="35." f="29.842" m="6.49602" t="0.226"/>\r
26 <eng-data cg="35." f="28.935" m="5.79035" t="0.275"/>\r
27 <eng-data cg="35." f="29.389" m="5.49025" t="0.296"/>\r
28 <eng-data cg="35." f="28.027" m="4.99787" t="0.331"/>\r
29 <eng-data cg="35." f="25.971" m="3.80712" t="0.421"/>\r
30 <eng-data cg="35." f="24.146" m="3.10718" t="0.478"/>\r
31 <eng-data cg="35." f="20.728" m="1.99669" t="0.579"/>\r
32 <eng-data cg="35." f="17.774" m="1.242" t="0.659"/>\r
33 <eng-data cg="35." f="14.356" m="0.612201" t="0.739"/>\r
34 <eng-data cg="35." f="9.569" m="0.260477" t="0.799"/>\r
35 <eng-data cg="35." f="4.557" m="0.0770365" t="0.852"/>\r
36 <eng-data cg="35." f="1.139" m="0.0114421" t="0.899"/>\r
37 <eng-data cg="35." f="0." m="0." t="0.94"/>\r
38 </data>\r
39 </engine>\r
40  </engine-list>\r
41 </engine-database>\r