version 1.0.0

[debian/openrocket] / datafiles / thrustcurves / AeroTech_F13.rse

diff --git a/datafiles/thrustcurves/AeroTech_F13.rse b/datafiles/thrustcurves/AeroTech_F13.rse
new file mode 100644 (file)
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+++ b/datafiles/thrustcurves/AeroTech_F13.rse
@@ -0,0 +1,46 @@
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="195.95" Itot="62.067" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="12.17" burn-time="5.1" cgDiv="10" cgFix="1" cgStep="-1." code="F13RCJ" delays="1000" dia="32." exitDia="0." initWt="110.5" len="107." mDiv="10" mFix="1" mStep="-1." massFrac="29.23" mfg="Aerotech" peakThrust="19.98" propWt="32.3" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech F13RCJ 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="53.5" f="0." m="32.3" t="0."/>\r
+<eng-data cg="53.5" f="15.309" m="32.1088" t="0.048"/>\r
+<eng-data cg="53.5" f="18.629" m="31.7909" t="0.084"/>\r
+<eng-data cg="53.5" f="19.98" m="31.1982" t="0.143"/>\r
+<eng-data cg="53.5" f="18.968" m="29.4956" t="0.311"/>\r
+<eng-data cg="53.5" f="18.172" m="27.3019" t="0.538"/>\r
+<eng-data cg="53.5" f="17.138" m="25.5471" t="0.729"/>\r
+<eng-data cg="53.5" f="15.428" m="23.3185" t="0.992"/>\r
+<eng-data cg="53.5" f="13.828" m="21.1337" t="1.279"/>\r
+<eng-data cg="53.5" f="12.456" m="18.4391" t="1.673"/>\r
+<eng-data cg="53.5" f="11.879" m="16.4698" t="1.984"/>\r
+<eng-data cg="53.5" f="12.227" m="16.0935" t="2.044"/>\r
+<eng-data cg="53.5" f="11.313" m="15.5116" t="2.139"/>\r
+<eng-data cg="53.5" f="11.193" m="14.112" t="2.378"/>\r
+<eng-data cg="53.5" f="11.084" m="13.3469" t="2.51"/>\r
+<eng-data cg="53.5" f="12.108" m="13.0572" t="2.558"/>\r
+<eng-data cg="53.5" f="10.855" m="12.5613" t="2.641"/>\r
+<eng-data cg="53.5" f="10.736" m="10.6793" t="2.976"/>\r
+<eng-data cg="53.5" f="10.627" m="7.82211" t="3.49"/>\r
+<eng-data cg="53.5" f="10.507" m="5.71596" t="3.873"/>\r
+<eng-data cg="53.5" f="10.965" m="5.0511" t="3.992"/>\r
+<eng-data cg="53.5" f="10.627" m="4.84884" t="4.028"/>\r
+<eng-data cg="53.5" f="10.507" m="2.74819" t="4.41"/>\r
+<eng-data cg="53.5" f="10.736" m="1.55979" t="4.625"/>\r
+<eng-data cg="53.5" f="9.941" m="0.785045" t="4.769"/>\r
+<eng-data cg="53.5" f="8.684" m="0.49427" t="4.829"/>\r
+<eng-data cg="53.5" f="6.742" m="0.349771" t="4.865"/>\r
+<eng-data cg="53.5" f="3.199" m="0.104039" t="4.96"/>\r
+<eng-data cg="53.5" f="1.485" m="0.0309119" t="5.02"/>\r
+<eng-data cg="53.5" f="0." m="0." t="5.1"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r