<?xml version="1.0"?>
<!-- 
  Vacuum Isp     445
  Sea Level Isp  
  Pc            610 psia
  Thrust        22,300 lbs Vac
  MR            5.5:1 (O:F)
  Design altitude 
-->
<rocket_engine name="RL-10">
  <isp>                   445  </isp>
  <maxthrottle>           1.0   </maxthrottle>
  <minthrottle>           1.0   </minthrottle>
  <slfuelflowmax unit="LBS/SEC">  7.71  </slfuelflowmax>
  <sloxiflowmax unit="LBS/SEC">   42.4  </sloxiflowmax>
</rocket_engine>
