The Superfluid Helium On-Orbit Transfer (SHOOT) Flight Demonstration w
as part of the space shuttle STS-57 mission in June, 1993. The experim
ent objectives included: transfer of superfluid between two dewars in
a low gravity environment at different flow rates; operation of two di
fferent liquid acquisition devices within the dewars; liquid/vapor pha
se separation for normal liquid helium as well as superfluid at varyin
g venting rates; accurate mass gauging and flow metering; and autonomo
us control of the transfer process by an expert system aboard a comput
er on the shuttle. This paper summarizes the findings of the SHOOT exp
eriment and the performance of individual components, with particular
emphasis on the anomalous behavior of one of the phase separators.