version 1.0.0

[debian/openrocket] / datafiles / thrustcurves / AeroTech_D21.rse

diff --git a/datafiles/thrustcurves/AeroTech_D21.rse b/datafiles/thrustcurves/AeroTech_D21.rse
new file mode 100644 (file)
index 0000000..e425c22
--- /dev/null
+++ b/datafiles/thrustcurves/AeroTech_D21.rse
@@ -0,0 +1,41 @@
+<engine-database>\r
+ <engine-list>\r
+<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
+<comments>Aerotech D21 RASP.ENG file made from NAR published data\r
+File produced July 4, 2000\r
+The total impulse, peak thrust, average thrust and burn time are\r
+the same as the averaged static test data on the NAR web site in\r
+the certification file. The curve drawn with these data points is as\r
+close to the certification curve as can be with such a limited\r
+number of points (32) allowed with wRASP up to v1.6.\r
+</comments>\r
+<data>\r
+<eng-data cg="35." f="0." m="9.6" t="0."/>\r
+<eng-data cg="35." f="1.367" m="9.59665" t="0.01"/>\r
+<eng-data cg="35." f="19.367" m="9.54077" t="0.021"/>\r
+<eng-data cg="35." f="32.12" m="9.43985" t="0.029"/>\r
+<eng-data cg="35." f="31.667" m="9.31481" t="0.037"/>\r
+<eng-data cg="35." f="30.528" m="9.10147" t="0.051"/>\r
+<eng-data cg="35." f="30.074" m="8.46298" t="0.094"/>\r
+<eng-data cg="35." f="31.213" m="8.14763" t="0.115"/>\r
+<eng-data cg="35." f="30.074" m="7.87734" t="0.133"/>\r
+<eng-data cg="35." f="30.76" m="7.2215" t="0.177"/>\r
+<eng-data cg="35." f="29.842" m="7.04331" t="0.189"/>\r
+<eng-data cg="35." f="30.528" m="6.83623" t="0.203"/>\r
+<eng-data cg="35." f="29.842" m="6.49602" t="0.226"/>\r
+<eng-data cg="35." f="28.935" m="5.79035" t="0.275"/>\r
+<eng-data cg="35." f="29.389" m="5.49025" t="0.296"/>\r
+<eng-data cg="35." f="28.027" m="4.99787" t="0.331"/>\r
+<eng-data cg="35." f="25.971" m="3.80712" t="0.421"/>\r
+<eng-data cg="35." f="24.146" m="3.10718" t="0.478"/>\r
+<eng-data cg="35." f="20.728" m="1.99669" t="0.579"/>\r
+<eng-data cg="35." f="17.774" m="1.242" t="0.659"/>\r
+<eng-data cg="35." f="14.356" m="0.612201" t="0.739"/>\r
+<eng-data cg="35." f="9.569" m="0.260477" t="0.799"/>\r
+<eng-data cg="35." f="4.557" m="0.0770365" t="0.852"/>\r
+<eng-data cg="35." f="1.139" m="0.0114421" t="0.899"/>\r
+<eng-data cg="35." f="0." m="0." t="0.94"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r