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http://lib.uliege.be https://matheo.uliege.be Scientific support for future space missions and multimethodological analysis of surface properties of solar system bodies Auteur : Romagnolo, Amedeo Promoteur(s) : Hubert, Benoit; 8567 Faculté : Faculté des Sciences Diplôme : Master en sciences spatiales, à finalité spécialisée Année académique : 2018-2019 URI/URL : http://hdl.handle.net/2268.2/8386 Avertissement à l'attention des usagers : Tous les documents placés en accès ouvert sur le site le site MatheO sont protégés par le droit d'auteur. Conformément aux principes énoncés par la "Budapest Open Access Initiative"(BOAI, 2002), l'utilisateur du site peut lire, télécharger, copier, transmettre, imprimer, chercher ou faire un lien vers le texte intégral de ces documents, les disséquer pour les indexer, s'en servir de données pour un logiciel, ou s'en servir à toute autre fin légale (ou prévue par la réglementation relative au droit d'auteur). 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Scientific support for future space missions and multimethodological analysis of surface properties of solar system bodies Master Thesis Sunday 15th September, 2019 MASTER DEGREE OF SPACE SCIENCES Author Amedeo Romagnolo (Student ID: 176733) Internal Supervisors Prof. Benoit Hubert Prof. Denis Grodent External Supervisor Dr. Ozgur Karatekin Examiners Prof. Véronique Dehant Prof. Emmanuël Jehin Ai miei nonni. Non passa giorno senza che non vi pensi. Se esiste qualcosa al di là di questa vita spero che possiate vedermi ed essere orgliosi della persona che sono diventato. Mi mancate immensamente. Abstract This thesis will include the two main projects collaborations done at the Royal Observatory of Belgium (ROB) as part of the internship started in March and lasted until mid-August 2019. The first project, with the collaboration of the Institut royal d’Aéronomie Spa- tiale de Belgique (BIRA·IASB), regarded the development of a data processing software to be used in the VIS-NIR detectors characterization for the Moon and Jupiter Imaging Spectrometer (MAJIS), which is one of the ten instruments con- stituting the ESA JUICE mission’s science payload. After a period of familiarization with Python programming language and a base- line software developed by ROB for UV observations, the data processing software was adopted to fully analyze and process the images from the MAJIS detector characterization. The validation of the software had been proved both by simu- lations from a model in collaboration with ROB, and (partially) by instrumental images obtained from the Institut d’Astrophysique Spatiale (IAS, France), which is leading the project. The second project was aimed at improving the general knowledge of the plane- tary ice caps spectroscopic analysis via the study of Martian north pole; this has been done both to contribute to the understanding of the planet’s climate via the analysis of the temporal evolution of H2O and CO2 polar ice, and to design a specific analysis software for spectroscopic data that could be used in the future for the MAJIS mission. After a new familiarization period with MATLAB and the baseline scripts from previous works, a full software capable of processing spectroscopic data from the Compact Reconnaissance Imaging Spectrometer for Mars (CRISM) and moni- toring the seasonal variations of the H2O and CO2 polar surface ice has been developed. The software has been partially validated with the literature, and the results suggest that an improvement has been done from the previous works in terms of processing time and noise reduction. Both the projects provided enough scientific data for a co-authorship into two different posters for the EPSC-DPS Joint Meeting 2019 in Geneva, Switzerland. Amedeo Romagnolo CONTENTS Contents 1 MAJIS Data Processing Software 1 1.1 Introduction . 1 1.2 The MAJIS experiment . 2 1.2.1 Jupiter . 2 1.2.2 Europa, Ganymede and Callisto . 3 1.2.3 Io, Rings and Small Satellites . 3 1.3 The Spectrometer . 4 1.3.1 Optical Design . 5 1.3.2 Spectral Performances . 5 1.3.3 Dichroic . 6 1.3.4 Gratings . 7 1.3.5 Scan Mirror Unit . 7 1.3.6 Internal Calibration Unit . 8 1.3.7 Teledyne Detectors . 8 1.3.8 Focal Planes . 8 1.4 The VIS-NIR Detectors Characterization . 9 1.4.1 The Facility . 9 1.4.2 The Configurations . 10 1.5 Characterization Procedure . 11 1.5.1 Photon Transfer Curve . 12 1.6 Characterization Parameters in Dark Conditions . 14 1.6.1 Dark Current (DC) . 14 1.6.2 Dark-Signal Non-Uniformity (DSNU) . 15 1.6.3 Read-Out Noise (RON) . 15 1.6.4 Power Dissipation . 16 1.7 Characterization Parameters in Light Conditions . 17 1.7.1 Useful Spectral Range . 19 1.7.2 Quantum Efficiency . 19 1.7.3 Full Well Capacity (FWC) . 21 1.7.4 Saturation . 21 1.7.5 Conversion Gain . 21 1.7.6 Linearity . 21 1.7.7 Defective Pixels and Cluster Mapping . 23 1.7.8 Photo-Response Non-Uniformity (PRNU) . 23 1.7.9 Operability . 23 1.7.10 Persistence . 24 1.7.11 Power Consumption . 25 I Amedeo Romagnolo CONTENTS 1.8 The Data Processing Software Development . 26 1.8.1 The Baseline Software . 26 1.8.2 The Work at ROB . 26 1.9 Results . 31 2 CRISM 35 2.1 Introduction . 35 2.2 Introduction to Mars . 36 2.3 The Instrument . 38 2.3.1 Observations . 39 2.4 Surface Ice Detection . 41 2.5 Baseline Software . 44 2.5.1 CRISM Software v2 . 44 2.5.2 CRISM Software v3 . 46 2.6 CRISM Software v4 Development . 49 2.6.1 Scripts Improvement . 49 2.6.2 Data Analysis . 50 2.7 CRISM Analysis Results . 53 3 Conclusions 56 II Amedeo Romagnolo LIST OF TABLES List of Figures 1 Czerny-Turner Configuration . 5 2 MAJIS Spectral Performances . 6 3 Dichroic Efficiency . 6 4 Gratings Efficiency . 7 5 Characterization Bench . 10 6 Characterization Measurements Diagram . 11 7 Photon Transfer Curve . 12 8 Non-Linearity Example . 22 9 Short Wave Pass Filter . 24 10 MAJIS Preliminary Simulations . 27 11 Corrected PTC . 28 12 Reference Columns Noise . 29 13 Reference Columns . 29 14 Corrected Reference Columns Noise . 30 15 Reference Columns Signal after Subtraction . 31 16 IAS-BIRA CDS Images Comparison . 32 17 Simulated Defective Pixel Clusters . 33 18 Simulated Persistence Pixel Color Map . 34 19 Martian Solar Longitude . 36 20 Martian Dust Annual Cycle . 37 21 CRISM Components . 38 22 CRISM Optics . 38 23 IAS Simulated Spectra . 41 24 Smile Effect . 45 25 Noisy Mars Polar Cap . 46 26 Noisy Mars Polar Cap Variability . 47 27 CO2 ice from Brown et al. 48 28 CO2 ice from Piqueux et al. 48 29 Comparison of Noise Attenuation Methods . 51 30 Perfect Sphere Distances Retrieval . 52 31 Ice Caps Temporal Evolution . 53 32 Complete Ice Caps Temporal Evolution . 53 33 Areas Comparison of Ice Caps . 54 List of Tables 1 Surface Ice Spectral Parameters . 43 III Amedeo Romagnolo 1 MAJIS DATA PROCESSING SOFTWARE 1 Data Processing Software for MAJIS VIS-NIR detectors Acknowledgements: [BIRA] David Bolsée, Miriam Cisneros, Nuno Pereira, Gaël Cessateur; [ROB] Boris Giordanengo, Samuel Gissot, [IAS] Paolo Haffoud, François Poulet, Yves Langevin 1.1 Introduction The Large Moons and Jupiter Imaging Spectrometer (MAJIS) is an instrument that will be part of the ESA Jupiter Icy Moons Explorer (JUICE), which is the first large-class mission of Cosmic Vision 2015-2025 [1]. The spacecraft is planned to be launched with either an Ariane 5 or an Ariane 64 launch vehicle in 2022 and reach Jupiter with gravity assist from Earth, Venus and Mars in 2029 [1, 2], with the goal of making detailed observation of the planet and its moons Ganymede, Callisto and Europa. The spacecraft will do several flybys around these bodies and will eventually insert in orbit around Ganymede. The mission will include ten state-of-the-art instruments and the spacecraft will host in its science payload eleven main experiments. 1 Amedeo Romagnolo 1 MAJIS DATA PROCESSING SOFTWARE 1.2 The MAJIS experiment With the Centre National d’Études Spatiales (CNES, France) as the leading fund- ing agency as the principal investigator, this experiment is a joint collaboration between several institutes, like the Institut d’Astrophysique Spatiale (IAS), the Istituto Nazionale di Astrofisica (INAS), the Institut royal d’Aéronomie Spatiale de Belgique (BIRA·IASB) [3], the Royal Observatory of Belgium (ROB) and the University of Liège. 1.2.1 Jupiter With an IFOV of 125 µrad MAJIS will be able to have a resolution of 125 km from Ganymede’s orbit [4]. In this conditions the full diameter of Jupiter will be continuously monitored with a coverage of 1070 pixels. The orbit of JUICE will also enable MAJIS to take measurements of the planet’s atmosphere in all local time conditions, not having therefore the coverage prob- lems that JUNO had [4]. Below, the reader can find the MAJIS scientific objective for the planet’s study. • Upper Atmosphere - Since the instrument will be capable of detecting + the H3 bands around 3.7 µm [4, 5], which interact with Jovian auroras, MAJIS will be able to monitor auroral activity and phenomenology and to make instantaneous mapping.