Improvement of the instrumental model for the MICROSCOPE space mission

Master thesis (2018)

Authors

Contributors

Ernst Schrama (mentor)

Manuel Rodrigues (mentor)

Faculty

Aerospace Engineering, Aerospace Engineering

Satellite data processing MICROSCOPE microsatellite Satellite Instrumentation Equivalence Principle test Electrostatic accelerometer Coupling defects Thermal sensitivity

To reference this document use:

http://resolver.tudelft.nl/uuid:df6c885f-a52f-488a-be7f-d05fe29e9f59

More Info

expand_more

Published Date

31-10-2018

Language

English

Reuse Rights

Other than for strictly personal use, it is not permitted to download, forward or distribute the text or part of it, without the consent of the author(s) and/or copyright holder(s), unless the work is under an open content license such as Creative Commons.

Faculty

Aerospace Engineering

Abstract

The Equivalence Principle is today challenged by some theories attempting to unify General Relativity and Quantum Mechanics. The MICROSCOPE mission thus intents to confirm or overturn this principle by testing the universality of free fall in space with an unrivaled precision objective of 10^-15. The principle of the test relies on the precise measurement of a gravitational signal by a differential electrostatic accelerometer (referred to as SAGE instrument) on board a drag-free microsatellite. The precision of the measurements exploited for the test is limited by several perturbations due to the high sensitivity of the instrument. The instrumental model implemented to process the collected data used overestimated models for some systematic errors such as the thermal sensitivity and coupling defects. The additional scientific measurements available by the end of the mission, will enable to perform a more in-depth exploration of these errors and thus to improve the current instrumental model. This is the purpose of this research work.

Files

MScThesis_FinalReport_Belis_46... (pdf)

(pdf | 7.42 Mb)

Unknown license