version 1.0.0

[debian/openrocket] / datafiles / thrustcurves / AeroTech_K680.rse

diff --git a/datafiles/thrustcurves/AeroTech_K680.rse b/datafiles/thrustcurves/AeroTech_K680.rse
new file mode 100644 (file)
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+++ b/datafiles/thrustcurves/AeroTech_K680.rse
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+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="182.74" Itot="2358.34" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="675.742" burn-time="3.49" cgDiv="10" cgFix="1" cgStep="-1." code="K680R" delays="1000" dia="98." exitDia="0." initWt="3035." len="289." mDiv="10" mFix="1" mStep="-1." massFrac="43.36" mfg="Aerotech" peakThrust="819.178" propWt="1316." tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<comments>Aerotech K680R RASP engine file\r
+Data Entered by Tim Van Milligan\r
+Source: TRA Certification paperwork, and\r
+Aerotech's instruction sheet: RMS 98/2560-10240 REDLINE.\r
+</comments>\r
+<data>\r
+<eng-data cg="144.5" f="0." m="1316." t="0."/>\r
+<eng-data cg="144.5" f="629.798" m="1301.06" t="0.085"/>\r
+<eng-data cg="144.5" f="717.881" m="1147.27" t="0.494"/>\r
+<eng-data cg="144.5" f="797.157" m="935.073" t="0.996"/>\r
+<eng-data cg="144.5" f="819.178" m="802.487" t="1.29"/>\r
+<eng-data cg="144.5" f="819.178" m="703.749" t="1.506"/>\r
+<eng-data cg="144.5" f="775.136" m="483.559" t="2.001"/>\r
+<eng-data cg="144.5" f="673.84" m="274.142" t="2.519"/>\r
+<eng-data cg="144.5" f="563.735" m="111.508" t="2.99"/>\r
+<eng-data cg="144.5" f="541.714" m="66.1689" t="3.137"/>\r
+<eng-data cg="144.5" f="532.906" m="54.4756" t="3.176"/>\r
+<eng-data cg="144.5" f="563.735" m="35.5052" t="3.238"/>\r
+<eng-data cg="144.5" f="563.735" m="23.5513" t="3.276"/>\r
+<eng-data cg="144.5" f="52.85" m="0.842942" t="3.408"/>\r
+<eng-data cg="144.5" f="22.02" m="0.362484" t="3.431"/>\r
+<eng-data cg="144.5" f="0." m="0." t="3.49"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r