DocumentCode :
976281
Title :
Spacecraft charging potential during electron-beam injections into space plasmas
Author :
Lin, Chin S. ; Koga, James
Author_Institution :
Dept. of Space Sci., Southwest Res. Inst., San Antonio, TX, USA
Volume :
17
Issue :
2
fYear :
1989
fDate :
4/1/1989 12:00:00 AM
Firstpage :
205
Lastpage :
209
Abstract :
Injections of nonrelativistic electron beams from an infinite conductor have been simulated by using a two-dimensional electrostatic particle code to study the spacecraft charging potential. The simulations show that the conductor charging potential at the end of simulations does not vary with the beam density when the beam density exceeds four times the ambient density. The reflection coefficient, which determines a percentage of incident electrons reflected by the conductor, increases the charging potential. To charge the conductor to the beam energy, the reflection coefficient needs to be about 0.5. The results are applied to explain the spacecraft charging potential measured during the SEPAC (Space Experiments with Particle Accelerators) experiments from Spacelab 1
Keywords :
electric potential; electron beam effects; ionosphere; plasma; plasma density; plasma-beam interactions; space vehicles; SEPAC; Space Experiments with Particle Accelerators; Spacelab 1; atmosphere; charging potential; conductor; density; electron-beam injections; ionosphere; nonrelativistic electron beams; reflection coefficient; space plasmas; space vehicles; spacecraft; two-dimensional electrostatic particle code; Conductors; Electron beams; Ionosphere; Optical reflection; Particle beams; Plasma accelerators; Plasma measurements; Plasma simulation; Space shuttles; Space vehicles;
fLanguage :
English
Journal_Title :
Plasma Science, IEEE Transactions on
Publisher :
ieee
ISSN :
0093-3813
Type :
jour
DOI :
10.1109/27.24626
Filename :
24626
Link To Document :
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