version 1.0.0

[debian/openrocket] / datafiles / thrustcurves / AeroTech_G55.rse

diff --git a/datafiles/thrustcurves/AeroTech_G55.rse b/datafiles/thrustcurves/AeroTech_G55.rse
new file mode 100644 (file)
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--- /dev/null
+++ b/datafiles/thrustcurves/AeroTech_G55.rse
@@ -0,0 +1,49 @@
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="195.08" Itot="119.567" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="49.003" burn-time="2.44" cgDiv="10" cgFix="1" cgStep="-1." code="G55" delays="5,10,15" dia="24." exitDia="0." initWt="114.8" len="117." mDiv="10" mFix="1" mStep="-1." massFrac="54.44" mfg="Aerotech" peakThrust="84.65" propWt="62.5" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech G55 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="58.5" f="0." m="62.5" t="0."/>\r
+<eng-data cg="58.5" f="81.136" m="62.3091" t="0.009"/>\r
+<eng-data cg="58.5" f="84.65" m="62.0925" t="0.014"/>\r
+<eng-data cg="58.5" f="80.557" m="61.2289" t="0.034"/>\r
+<eng-data cg="58.5" f="77.064" m="59.1691" t="0.084"/>\r
+<eng-data cg="58.5" f="71.823" m="57.3791" t="0.13"/>\r
+<eng-data cg="58.5" f="72.422" m="55.4941" t="0.18"/>\r
+<eng-data cg="58.5" f="68.919" m="54.5337" t="0.206"/>\r
+<eng-data cg="58.5" f="69.538" m="49.6122" t="0.342"/>\r
+<eng-data cg="58.5" f="68.989" m="44.5073" t="0.483"/>\r
+<eng-data cg="58.5" f="66.663" m="43.4436" t="0.513"/>\r
+<eng-data cg="58.5" f="68.42" m="42.3845" t="0.543"/>\r
+<eng-data cg="58.5" f="66.114" m="38.1299" t="0.664"/>\r
+<eng-data cg="58.5" f="66.164" m="30.8006" t="0.876"/>\r
+<eng-data cg="58.5" f="64.418" m="29.9474" t="0.901"/>\r
+<eng-data cg="58.5" f="65.026" m="26.6996" t="0.997"/>\r
+<eng-data cg="58.5" f="66.793" m="24.4602" t="1.062"/>\r
+<eng-data cg="58.5" f="63.879" m="23.5722" t="1.088"/>\r
+<eng-data cg="58.5" f="63.889" m="21.5686" t="1.148"/>\r
+<eng-data cg="58.5" f="66.813" m="21.227" t="1.158"/>\r
+<eng-data cg="58.5" f="63.31" m="20.7169" t="1.173"/>\r
+<eng-data cg="58.5" f="62.741" m="19.5308" t="1.209"/>\r
+<eng-data cg="58.5" f="61.593" m="15.7613" t="1.325"/>\r
+<eng-data cg="58.5" f="59.277" m="13.55" t="1.395"/>\r
+<eng-data cg="58.5" f="57.541" m="11.6875" t="1.456"/>\r
+<eng-data cg="58.5" f="58.129" m="10.7806" t="1.486"/>\r
+<eng-data cg="58.5" f="52.32" m="7.86504" t="1.587"/>\r
+<eng-data cg="58.5" f="40.094" m="4.94249" t="1.708"/>\r
+<eng-data cg="58.5" f="26.11" m="2.93533" t="1.824"/>\r
+<eng-data cg="58.5" f="15.63" m="1.56077" t="1.95"/>\r
+<eng-data cg="58.5" f="7.498" m="0.581525" t="2.112"/>\r
+<eng-data cg="58.5" f="3.446" m="0.163918" t="2.258"/>\r
+<eng-data cg="58.5" f="0." m="0." t="2.44"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r