PSP Bibliography





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Found 3 entries in the Bibliography.


Showing entries from 1 through 3


2014

Cross-comparison of spacecraft-environment interaction model predictions applied to Solar Probe Plus near perihelion

Five spacecraft-plasma models are used to simulate the interaction of a simplified geometry Solar Probe Plus (SPP) satellite with the space environment under representative solar wind conditions near perihelion. By considering similarities and differences between results obtained with different numerical approaches under well defined conditions, the consistency and validity of our models can be assessed. The impact on model predictions of physical effects of importance in the SPP mission is also considered by comparing re ...

Marchand, R.; Miyake, Y.; Usui, H.; Deca, J.; Lapenta, G.; elez, J.; Ergun, R.; Sturner, A.; enot, V.; Hilgers, A.; Markidis, S.;

Published by: Physics of Plasmas      Published on: 06/2014

YEAR: 2014     DOI: 10.1063/1.4882439

Parker Data Used; parker solar probe; Solar Probe Plus

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: DEC

YEAR: 2013     DOI: 10.1109/TPS.2013.2246193

Parker Data Used

2012

Solar wind plasma interaction with solar probe plus spacecraft

3-D PIC (Particle In Cell) simulations of spacecraft-plasma interactions in the solar wind context of the Solar Probe Plus mission are presented. The SPIS software is used to simulate a simplified probe in the near-Sun environment (at a distance of 0.044 AU or 9.5 RS from the Sun surface). We begin this study with a cross comparison of SPIS with another PIC code, aiming at providing the static potential structure surrounding a spacecraft in a high photoelectron environment. This paper presents then a s ...

Guillemant, S.; enot, V.; elez, J.-C.; Ergun, R.; Louarn, P.;

Published by: Annales Geophysicae      Published on: 07/24/2012

YEAR: 2012     DOI: 10.5194/angeo-30-1075-2012

Parker Data Used; Solar Probe Plus



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