X-Git-Url: https://git.gag.com/?a=blobdiff_plain;f=datafiles%2Fthrustcurves%2FAeroTech_I154.rse;fp=datafiles%2Fthrustcurves%2FAeroTech_I154.rse;h=af341650bd589b181ae4f7b5ff254b0d8bc49e6b;hb=bf76931b27b597f7bc1dd5a0e7e2460ac065415b;hp=0000000000000000000000000000000000000000;hpb=def27b03bd9ebe6628421ec61112ebe4f45f043d;p=debian%2Fopenrocket

diff --git a/datafiles/thrustcurves/AeroTech_I154.rse b/datafiles/thrustcurves/AeroTech_I154.rse
new file mode 100644
index 00000000..af341650
--- /dev/null
+++ b/datafiles/thrustcurves/AeroTech_I154.rse
@@ -0,0 +1,22 @@
+<engine-database>
+ <engine-list>
+<engine FDiv="10" FFix="1" FStep="-1." Isp="140.33" Itot="385.327" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="107.035" burn-time="3.6" cgDiv="10" cgFix="1" cgStep="-1." code="I154J" delays="6,10" dia="38." exitDia="0." initWt="506.3" len="250." mDiv="10" mFix="1" mStep="-1." massFrac="55.3" mfg="Aerotech" peakThrust="199.49" propWt="280." tDiv="10" tFix="1" tStep="-1." throatDia="0.">
+<data>
+<eng-data cg="125." f="0." m="280." t="0."/>
+<eng-data cg="125." f="199.49" m="280." t="0."/>
+<eng-data cg="125." f="162.84" m="266.836" t="0.1"/>
+<eng-data cg="125." f="153.9" m="243.819" t="0.3"/>
+<eng-data cg="125." f="149.32" m="232.803" t="0.4"/>
+<eng-data cg="125." f="149.32" m="211.102" t="0.6"/>
+<eng-data cg="125." f="126.72" m="170.985" t="1."/>
+<eng-data cg="125." f="117.65" m="117.713" t="1.6"/>
+<eng-data cg="125." f="113.11" m="109.329" t="1.7"/>
+<eng-data cg="125." f="113.11" m="76.4518" t="2.1"/>
+<eng-data cg="125." f="95.05" m="38.6366" t="2.6"/>
+<eng-data cg="125." f="67.88" m="9.03814" t="3.1"/>
+<eng-data cg="125." f="22.6" m="2.46336" t="3.3"/>
+<eng-data cg="125." f="0." m="0." t="3.6"/>
+</data>
+</engine>
+ </engine-list>
+</engine-database>