X-Git-Url: https://git.gag.com/?a=blobdiff_plain;f=datafiles%2Fthrustcurves%2FAeroTech_J275.rse;fp=datafiles%2Fthrustcurves%2FAeroTech_J275.rse;h=0b750b2f764347c05bdc814a51e909545e4c3fb3;hb=bf76931b27b597f7bc1dd5a0e7e2460ac065415b;hp=0000000000000000000000000000000000000000;hpb=def27b03bd9ebe6628421ec61112ebe4f45f043d;p=debian%2Fopenrocket

diff --git a/datafiles/thrustcurves/AeroTech_J275.rse b/datafiles/thrustcurves/AeroTech_J275.rse
new file mode 100644
index 00000000..0b750b2f
--- /dev/null
+++ b/datafiles/thrustcurves/AeroTech_J275.rse
@@ -0,0 +1,22 @@
+<engine-database>
+ <engine-list>
+<engine FDiv="10" FFix="1" FStep="-1." Isp="189.65" Itot="818.693" Type="reloadable" auto-calc-cg="1" auto-calc-mass="1" avgThrust="255.842" burn-time="3.2" cgDiv="10" cgFix="1" cgStep="-1." code="J275W" delays="6,10,14,18" dia="54." exitDia="0." initWt="882.9" len="241." mDiv="10" mFix="1" mStep="-1." massFrac="49.86" mfg="Aerotech" peakThrust="350.5" propWt="440.2" tDiv="10" tFix="1" tStep="-1." throatDia="0.">
+<data>
+<eng-data cg="120.5" f="0." m="440.2" t="0."/>
+<eng-data cg="120.5" f="0.45" m="440.2" t="0."/>
+<eng-data cg="120.5" f="331.55" m="431.274" t="0.1"/>
+<eng-data cg="120.5" f="293.61" m="414.467" t="0.2"/>
+<eng-data cg="120.5" f="326.8" m="331.071" t="0.7"/>
+<eng-data cg="120.5" f="350.5" m="221.818" t="1.3"/>
+<eng-data cg="120.5" f="350.5" m="165.281" t="1.6"/>
+<eng-data cg="120.5" f="307.85" m="76.7843" t="2.1"/>
+<eng-data cg="120.5" f="269.99" m="45.7146" t="2.3"/>
+<eng-data cg="120.5" f="227.34" m="32.3442" t="2.4"/>
+<eng-data cg="120.5" f="85.27" m="7.13133" t="2.7"/>
+<eng-data cg="120.5" f="47.37" m="3.5654" t="2.8"/>
+<eng-data cg="120.5" f="9.47" m="0.509189" t="3."/>
+<eng-data cg="120.5" f="0." m="0." t="3.2"/>
+</data>
+</engine>
+ </engine-list>
+</engine-database>