PSP Bibliography





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2013

Simulation Study of Spacecraft Electrostatic Sheath Changes With the Heliocentric Distances from 0.044 to 1 AU

In this paper, the electrostatic sheath of a simplified spacecraft is investigated for heliocentric distances varying from 0.044 to 1 AU, using the 3-D Particle in Cell software Satellite-Plasma Interaction System. The baseline context is the prediction of sheath effects on solar wind measurements for various missions, including the Solar Probe Plus mission (perihelion at 0.044 AU from the sun) and Solar Orbiter (SO) (perihelion at 0.28 AU). The electrostatic sheath and the spacecraft potential could interfere with the low-e ...

Guillemant, Stanislas; Genot, Vincent; Velez, Jean-Charles; Sarrailh, Pierre; Hilgers, Alain; Louarn, Philippe;

Published by: IEEE TRANSACTIONS ON PLASMA SCIENCE      Published on: 12/2013

YEAR: 2013     DOI: 10.1109/TPS.2013.2246193

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