The atmospheric flow on Io is numerically computed in a hat 2-D axisym
metric geometry for a sublimation atmosphere on the trailing hemispher
e subjected to plasma bombardment, UV heating, and IR cooling. Calcula
tions are performed for subsolar vapor pressures of similar to 6.5 x 1
0(-3) Pa (similar to 3 x 10(18) SO2/cm(2)) and 6.8 x 10(-4) Pa (simila
r to 4 x 10(17) SO2/cm(2)); the latter approximates the vapor pressure
of F. P. Fanale et al. (1982, Satellites of Jupiter, pp. 756-781, Uni
v. of Arizona Press, Tucson). The amount of plasma energy deposited in
the atmosphere is 20% of the plasma dow energy due to corotation (J.
A. Linker et al., 1988, Geophys. Res. Lett. 15, 1311-3141). It is foun
d that plasma heating significantly inflates the upper atmosphere, inc
reasing both the exobase altitude and the amount of surface covered by
more than an exospheric column of gas. This in turn controls the supp
ly of the Io plasma torus (M. A. McGrath and R. E. Johnson, 1987, Icar
us 69, 519-531). The horizontal flow of mass and energy is also import
ant in determining the exobase altitude; and it is shown that IR cooli
ng can be important, although our use of the equilibrium, cool-to-spac
e approximation for a pure SO2 gas (E. Lellouch et al., 1992, Icarus 9
8, 271-295) may overestimate this effect. The calculated exobase altit
udes are somewhat lower than those suggested by McGrath and Johnson (1
987) for supplying the torus, indicating the details of the plasma ene
rgy deposition and sputter ejection rate near the exobase, as well as
the IR emission from this region need to be examined. In addition, the
molecules sublimed (or sputtered) from the surface are transported to
the exobase in times short compared to the molecular photodissociatio
n time. Therefore, the exobase is dominated by molecular species and t
he exobase is supplied by a small region of the surface. (C) 1995 Acad
emic Press, Inc.