The Superfluid Helium On-Orbit Transfer (SHOOT) project was a shuttle
payload designed to demonstrate the technology needed to transfer supe
rfluid helium between two Dewars in space. It was launched with normal
liquid helium which was pumped to superfluid temperatures on-orbit. D
uring the 93h prelaunch ground hold, the liquid was thermally stratifi
ed, with temperatures of almost-equal-to 4.3 K at the top and rising s
lowly from 2.2K at the bottom of each Dewar over time. This stratifica
tion was helpful, as it allowed for more efficient removal of the para
sitic heat inputs. There were also temperature gradients in the Dewars
during the on-orbit pumpdown, with a much higher degree of beneficial
stratification in the port Dewar than in the starboard. We describe t
he liquid temperature profiles during ground hold and on-orbit pumpdow
n, discussing the effects of this stratification and comparing the per
formances of the two Dewars. We also discuss the results of a computer
model of the isothermal pumpdown of a SHOOT Dewar on-orbit.