L'instrument AMBRE 1 (Active Monitor Box of Electrostatic Risks) est un spectromètre de mesure du plasma (ions positifs et électrons) composé de deux têtes de mesure qui a été lancé à bord du satellite Jason 3 en Janvier 2016. A travers la mesure du plasma thermique (énergies comprises entre ~0 et 35 keV) cet instrument permet, d'une part, de déterminer la charge électrostatique des satellites et les populations en étant à l'origine pour répondre à des enjeux opérationnels, et d'autre part, de caractériser les environnements plasma magnétosphériques avec des enjeux scientifiques. La réduction des caractéristiques physiques (poids, consommation électrique et encombrement) des instruments AMBRE est un enjeu clé dans le but de rendre son embarquement systématique sur les plateformes satellites (scientifiques comme commerciales) et ainsi étendre le réseau de ce type de mesures dans l'environnement terrestre. L'objectif de cette thèse porte sur la conception, le développement et la réalisation d'un prototype d'instrument AMBRE 2 répondant à ces enjeux, tout en améliorant les performances scientifiques. Cette nouvelle génération d'instrument repose sur l'utilisation d'une seule tête qui mesure les deux types de population de manière alternée dans le temps. L'étude de chaque sous-système d'AMBRE 2 a permis de trouver les meilleurs compromis permettant de mesurer les deux types de population tout en minimisant les ressources allouées à l'instrument. Un prototype a été réalisé et testé sous vide avec un canon à ions et un canon à électron courant octobre 2017 afin de valider son principe de fonctionnement. / The Active Monitor Box of Electrostatic Risks (AMBER) is a double-head thermal plasma (positive ions and electrons) electrostatic analyser that was launched onboard the Jason-3 spacecraft in January 2016. By measuring the thermal plasma (in the energy range ~0 - 45 keV) the instrument permits, on the one hand, to determine the spacecraft electrostatic charging and the populations at its origin with operational stakes, and, on the other hand, to characterize the magnetospheric plasma environments with scientific goals. Reducing the physical resources (weight, electric consumption, and volume) of the AMBRE line of instrument is key to a potential systematic embarkation onboard various platforms (scientific or commercial), thereby augmenting the constellation of such measurements in near-Earth space. The goal of the present thesis is to conceive, develop and build an AMBRE 2 instrument prototype that meets these goals while augmenting its scientific capabilities. This new generation of instrument relies on the use of a single head which alternatively measures ions and electrons. Each AMBRE 2 sub-system was studied and designed using the best trade-off solution between overall resources and capabilities. A prototype has been built and tested in a vacuum chamber with ion and electron beams in October 2017 in order to validate its functionality.

This thesis presents a study of the inner plasma disk of Saturn. The results are derived from measurements by the instruments on board the Cassini spacecraft, mainly the Cassini Langmuir probe (LP), which has been in orbit around Saturn since 2004. One of the great discoveries of the Cassini spacecraft is that the Saturnian moon Enceladus, located at 3.95 Saturn radii (1 RS = 60,268 km), constantly expels water vapor and condensed water from ridges and troughs located in its south polar region. Impact ionization and photoionization of the water molecules, and subsequent transport, creates a plasma disk around the orbit of Enceladus. The plasma disk ion components are mainly hydrogen ions H+ and water group ions W+ (O+, OH+, H2O+, and H3O+). The Cassini LP is used to measure the properties of the plasma. A new method to derive ion density and ion velocity from Langmuir probe measurements has been developed. The estimated LP statistics are used to derive the extension of the plasma disk, which show plasma densities above ~20 cm-3 in between 2.7 and 8.8 RS. The densities also show a very variable plasma disk, varying with one order of magnitude at the inner part of the disk. We show that the density variation could partly be explained by a dayside/nightside asymmetry in both equatorial ion densities and azimuthal ion velocities. The asymmetry is suggested to be due to the particle orbits being shifted towards the Sun that in turn would cause the whole plasma disk to be shifted. We also investigate the ion loss processes of the inner plasma disk and conclude that loss by transport dominates loss by recombination in the entire region. However, loss by recombination is still important in the region closest to Enceladus (~±0.5 RS) where it differs with only a factor of two from ion transport loss.