version 1.0.0
[debian/openrocket] / datafiles / thrustcurves / AeroTech_D7.rse
1 <engine-database>\r
2  <engine-list>\r
3 <engine FDiv="10" FFix="1" FStep="-1." Isp="179.93" Itot="18.527" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="6.456" burn-time="2.87" cgDiv="10" cgFix="1" cgStep="-1." code="D7RC" delays="1000" dia="24." exitDia="0." initWt="42.2" len="70." mDiv="10" mFix="1" mStep="-1." massFrac="24.88" mfg="Aerotech " peakThrust="10.99" propWt="10.5" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
4 <comments>Aerotech D7 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="10.5" t="0."/>\r
14 <eng-data cg="35." f="3.336" m="10.466" t="0.036"/>\r
15 <eng-data cg="35." f="9.326" m="10.2937" t="0.084"/>\r
16 <eng-data cg="35." f="10.281" m="10.1993" t="0.101"/>\r
17 <eng-data cg="35." f="10.827" m="9.94808" t="0.143"/>\r
18 <eng-data cg="35." f="10.99" m="9.51533" t="0.213"/>\r
19 <eng-data cg="35." f="10.887" m="9.15578" t="0.271"/>\r
20 <eng-data cg="35." f="10.685" m="8.61786" t="0.359"/>\r
21 <eng-data cg="35." f="10.13" m="7.95726" t="0.471"/>\r
22 <eng-data cg="35." f="10.342" m="7.75423" t="0.506"/>\r
23 <eng-data cg="35." f="9.929" m="7.58765" t="0.535"/>\r
24 <eng-data cg="35." f="8.697" m="6.13621" t="0.81"/>\r
25 <eng-data cg="35." f="6.713" m="4.31969" t="1.226"/>\r
26 <eng-data cg="35." f="5.138" m="3.10068" t="1.589"/>\r
27 <eng-data cg="35." f="4.861" m="2.50285" t="1.8"/>\r
28 <eng-data cg="35." f="4.581" m="1.56374" t="2.151"/>\r
29 <eng-data cg="35." f="4.57" m="0.272392" t="2.649"/>\r
30 <eng-data cg="35." f="3.887" m="0.15976" t="2.696"/>\r
31 <eng-data cg="35." f="2.388" m="0.0672987" t="2.748"/>\r
32 <eng-data cg="35." f="0.889" m="0.0125122" t="2.807"/>\r
33 <eng-data cg="35." f="0.207" m="0.00164238" t="2.842"/>\r
34 <eng-data cg="35." f="0." m="0." t="2.87"/>\r
35 </data>\r
36 </engine>\r
37  </engine-list>\r
38 </engine-database>\r