<object-stream>
<com.billkuker.rocketry.motorsim.Motor>
<chamber class="com.billkuker.rocketry.motorsim.CylindricalChamber">
<ID>30 mm</ID>
<length>200 mm</length>
</chamber>
<fuel class="com.billkuker.rocketry.motorsim.fuel.KNSU"/>
<grain class="com.billkuker.rocketry.motorsim.grain.Finocyl">
<ID>10 mm</ID>
<OD>30 mm</OD>
<aftEndInhibited>false</aftEndInhibited>
<finCount>5</finCount>
<finDiameter>20 mm</finDiameter>
<finWidth>2 mm</finWidth>
<foreEndInhibited>false</foreEndInhibited>
<length>170 mm</length>
</grain>
<name>Example Motor</name>
<nozzle class="com.billkuker.rocketry.motorsim.ConvergentDivergentNozzle">
<efficiency>0.85</efficiency>
<exitDiameter>20 mm</exitDiameter>
<throatDiameter>15 mm</throatDiameter>
</nozzle>
</com.billkuker.rocketry.motorsim.Motor>
</object-stream>