A three-dimensional, time-dependent, two species (i.e. electron and io
n) particle simulation model gis developed for a better understanding
of current collection by a charged body in space. The Low Earth Orbit
(LEO) space environment is simulated by a super-particle simulation (S
UPS) model to study the plasma transient response and its asymptotic b
ehavior around a three-dimensional, highly biased satellite. The SUPS
model is developed because the plasma particles in LEGS are so abundan
t that it is impossible to simulate each single particle in the study.
Each simulation particle in this study represents a particle cloud. T
he potential distribution and the electric field are dependent on the
density distribution of the particles. The simulation could apply to t
he spacecraft mission such as the first Tether Satellite System Re-fly
(TSS-1R) mission for current collection analysis. Both positive and n
egative charged particles are considered in the study. The potential d
istribution surrounding the satellite is determined self-consistently
by Poisson's equation. This study is both time dependent and space dep
endent simultaneously. Results indicate that when the satellite is cha
rged to a highly positive potential, a plasma torus is formed in the p
lane perpendicular to the geomagnetic field. A dumbbell-shaped potenti
al distribution is formed along the geomagnetic field lines and plasma
oscillations are observed within the plasma sheath during the early s
tage of simulation. The effect of the local geomagnetic held on curren
t collection is also presented. (C) 1997 Elsevier Science Ltd.