An experiment, Astra-2, was performed at the space station Mir in 1995-1996
to study its ambient atmosphere parameters. For far-field plume research,
the equipment of Astra-2 included a small cold gas thruster using a marked
gas, argon. The results of this research offer a good basis for validation
of various numerical approaches for plume flows, from simple engineering mo
dels to exact numerical approaches using a Navier-Stokes solver in the cont
inuum regime and a direct simulation Monte-Carlo code in the near-continuum
, transitional, and free-molecular regimes. A comparison of experimental an
d numerical results shows the necessity of accounting for argon condensatio
n processes in the nozzle and in the vicinity near the nozzle.