Hi All,

Whilst browsing through the XCOR Reference Library
(accessible through a link on www.xcor.com) I
meandered my way over to a nasa tech briefs discussion
about vortex fuel mixing for rocket engines.  

<http://www.nasatech.com/Briefs/Sept00/MFS31477.html>

The idea sounds pretty cool.  Perhaps this could be
used in lieu of cooling passages for a bi-prop design.
 Thoughts?

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