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Spacecraft charging potential during electron-beam injections into space plasmas

机译:电子束注入太空等离子体期间的航天器充电电位

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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.
机译:通过使用二维静电粒子代码来研究航天器的充电电势,已经模拟了从无限导体注入非相对论性电子束的情况。仿真表明,当束密度超过环境密度的四倍时,在仿真结束时导体的充电电位不会随束密度而变化。反射系数决定了导体反射的入射电子的百分比,从而增加了充电电位。为了使导体充以束能量,反射系数需要约为0.5。该结果将用于解释在太空实验室1进行的SEPAC(带有粒子加速器的太空实验)实验中测得的航天器充电电位。

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