--- /dev/null
+<engine-database>\r
+ <engine-list>\r
+<engine FDiv="10" FFix="1" FStep="-1." Isp="202.87" Itot="1279.8" Type="single-use" auto-calc-cg="1" auto-calc-mass="1" avgThrust="124.98" burn-time="10.24" cgDiv="10" cgFix="1" cgStep="-1." code="J125W" delays="100" dia="54." exitDia="0." initWt="1115." len="368." mDiv="10" mFix="1" mStep="-1." massFrac="57.7" mfg="Aerotech" peakThrust="214." propWt="643.3" tDiv="10" tFix="1" tStep="-1." throatDia="0.">\r
+<data>\r
+<eng-data cg="184." f="0." m="643.3" t="0."/>\r
+<eng-data cg="184." f="214." m="589.516" t="1."/>\r
+<eng-data cg="184." f="200." m="381.416" t="3."/>\r
+<eng-data cg="184." f="142." m="294.602" t="4.01"/>\r
+<eng-data cg="184." f="120." m="97.7165" t="7."/>\r
+<eng-data cg="184." f="0." m="0." t="10.24"/>\r
+</data>\r
+</engine>\r
+ </engine-list>\r
+</engine-database>\r