version 1.0.0

[debian/openrocket] / datafiles / thrustcurves / Cesaroni_I216.rse

diff --git a/datafiles/thrustcurves/Cesaroni_I216.rse b/datafiles/thrustcurves/Cesaroni_I216.rse
new file mode 100644 (file)
index 0000000..bf95a6e
--- /dev/null
+++ b/datafiles/thrustcurves/Cesaroni_I216.rse
@@ -0,0 +1,31 @@
+<engine-database>\r
+  <engine-list>\r
+    <engine  mfg="CTI" code="I216-CL(I)" Type="reloadable" dia="38." len="367." initWt="601."\r
+propWt="312.5" delays="5,7,9,11,14" auto-calc-mass="1" auto-calc-cg="1"\r
+avgThrust="205.198" peakThrust="345." throatDia="0." exitDia="0." Itot="636.114"\r
+burn-time="3.1" massFrac="52." Isp="207.57" tDiv="10" tStep="-1." tFix="1"\r
+FDiv="10" FStep="-1." FFix="1" mDiv="10" mStep="-1." mFix="1" cgDiv="10"\r
+cgStep="-1." cgFix="1">\r
+    <comments>This motor is a standard Pro38-5G with a different nozzle to keep total impulse in 'I' range</comments>\r
+    <data>\r
+      <eng-data  t="0." f="0." m="312.5" cg="183.5"/>\r
+      <eng-data  t="0.017" f="35." m="312.354" cg="183.5"/>\r
+      <eng-data  t="0.03" f="300." m="311.284" cg="183.5"/>\r
+      <eng-data  t="0.035" f="345." m="310.492" cg="183.5"/>\r
+      <eng-data  t="0.05" f="325." m="308.023" cg="183.5"/>\r
+      <eng-data  t="0.07" f="275." m="305.076" cg="183.5"/>\r
+      <eng-data  t="0.14" f="292." m="295.327" cg="183.5"/>\r
+      <eng-data  t="0.26" f="296." m="277.995" cg="183.5"/>\r
+      <eng-data  t="0.8" f="280." m="201.593" cg="183.5"/>\r
+      <eng-data  t="1.1" f="280.4" m="160.298" cg="183.5"/>\r
+      <eng-data  t="1.62" f="255." m="91.9118" cg="183.5"/>\r
+      <eng-data  t="1.8" f="226." m="70.645" cg="183.5"/>\r
+      <eng-data  t="2.105" f="210." m="37.9809" cg="183.5"/>\r
+      <eng-data  t="2.2" f="195." m="28.5302" cg="183.5"/>\r
+      <eng-data  t="2.45" f="80." m="11.643" cg="183.5"/>\r
+      <eng-data  t="2.75" f="36." m="3.09496" cg="183.5"/>\r
+      <eng-data  t="3.1" f="0." m="0." cg="183.5"/>\r
+    </data>\r
+  </engine>\r
+</engine-list>\r
+</engine-database>\r