The direct simulation Monte Carlo method was applied to the analysis o
f low-density nitrogen plumes exhausting from a small converging-diver
ging nozzle into finite ambient pressures. Two cases were considered t
hat simulated actual test conditions in a vacuum facility. The numeric
al simulations readily captured the complicated flow structure of the
overexpanded plumes adjusting to the finite ambient pressures, includi
ng Mach disks and barrel-shaped shocks. The numerical simulations comp
ared well to experimental data of Rothe.