Published March 2009 | Version v1
Journal article

Odyssey: a Solar System Mission

Others:
DPHY, ONERA, Université Paris Saclay (COmUE) [Châtillon] ; ONERA-Université Paris Saclay (COmUE)
University of Oslo (UiO)
Global Aerospace ; Global Aerospace
Jet Propulsion Laboratory (JPL) ; NASA-California Institute of Technology (CALTECH)
Observatoire de la Côte d'Azur (OCA) ; Institut national des sciences de l'Univers (INSU - CNRS)-Centre National de la Recherche Scientifique (CNRS)
Astrophysique Relativiste Théories Expériences Métrologie Instrumentation Signaux (ARTEMIS) ; Université Nice Sophia Antipolis (1965 - 2019) (UNS) ; COMUE Université Côte d'Azur (2015-2019) (COMUE UCA)-COMUE Université Côte d'Azur (2015-2019) (COMUE UCA)-Institut national des sciences de l'Univers (INSU - CNRS)-Observatoire de la Côte d'Azur ; COMUE Université Côte d'Azur (2015-2019) (COMUE UCA)-Université Côte d'Azur (UCA)-Université Côte d'Azur (UCA)-Centre National de la Recherche Scientifique (CNRS)
Departamento de Física e Astronomia [Porto] (DFA/FCUP) ; Faculdade de Ciências da Universidade do Porto (FCUP) ; Universidade do Porto = University of Porto-Universidade do Porto = University of Porto
Instituto Superior Técnico ; Technical University of Lisbon
STFC Rutherford Appleton Laboratory (RAL) ; Science and Technology Facilities Council (STFC)
Institut d'Optique Graduate School (IOGS)
Center of Applied Space Technology and Microgravity (ZARM) ; Universität Bremen
Laboratoire Kastler Brossel (LKB (Jussieu)) ; Fédération de recherche du Département de physique de l'Ecole Normale Supérieure - ENS Paris (FRDPENS) ; École normale supérieure - Paris (ENS-PSL) ; Université Paris sciences et lettres (PSL)-Université Paris sciences et lettres (PSL)-Centre National de la Recherche Scientifique (CNRS)-École normale supérieure - Paris (ENS-PSL) ; Université Paris sciences et lettres (PSL)-Université Paris sciences et lettres (PSL)-Centre National de la Recherche Scientifique (CNRS)-Sorbonne Université (SU)-Centre National de la Recherche Scientifique (CNRS)
Astrium, Friedrichshafen,
Berkeley Radio Astronomy Laboratory (RAL) ; Department of Astronomy [Berkeley] ; University of California [Berkeley] (UC Berkeley) ; University of California (UC)-University of California (UC)-University of California [Berkeley] (UC Berkeley) ; University of California (UC)-University of California (UC)
Géoazur (GEOAZUR 7329) ; Institut national des sciences de l'Univers (INSU - CNRS)-Observatoire de la Côte d'Azur ; COMUE Université Côte d'Azur (2015-2019) (COMUE UCA)-Université Côte d'Azur (UCA)-COMUE Université Côte d'Azur (2015-2019) (COMUE UCA)-Université Côte d'Azur (UCA)-Centre National de la Recherche Scientifique (CNRS)-Institut de Recherche pour le Développement (IRD [France-Sud])
Joint Institute for VLBI in Europe (JIVE ERIC)
Imperial College London
ONERA, Université Paris Saclay (COmUE) [Palaiseau] ; ONERA-Université Paris Saclay (COmUE)
Systèmes de Référence Temps Espace (SYRTE) ; Université Pierre et Marie Curie - Paris 6 (UPMC)-Institut national des sciences de l'Univers (INSU - CNRS)-Observatoire de Paris ; Université Paris sciences et lettres (PSL)-Université Paris sciences et lettres (PSL)-Centre National de la Recherche Scientifique (CNRS)

Description

The Solar System Odyssey mission uses modern-day high-precision experimental techniques to answer some of the important questions on the laws of fundamental physics which determine dynamics in the solar system. It could lead to a major discovery by using readily available technologies and could be flown early within the Cosmic Vision time frame. The mission proposes to perform a set of precision gravitation experiments from the vicinity of Earth to the deep Solar System far beyond the orbit of known planets: verification of gravity in the deep Solar System, measurement of Eddington's parameter, investigation on fly-by anomaly, mapping of gravity field in the outer solar system. The Odyssey mission focuses its efforts on the challenge of designing a deep space mission within the cost of 300Meuros. This challenge restricts the main mission design choices (launcher, energy and payload options) and trade-offs in science goals. The payload definition emphasises demonstrated technology, with non gravitational forces measured by an accelerometer upgraded from an existing qualified design, and the probe followed by Doppler tracking and ranging built up on existing radio science instruments. In the baseline concept, the main spacecraft will fly beyond the Saturn orbit (up to 13 AU), with several fly-by, allowing the achievement of the first three scientific objectives. After the last fly-by, a radio-beacon is released and continues the mission up to at least 50 AU, with the extension of the deep space gravity experiment to larger distances and with achievement of the last scientific objective of the outer Solar System gravity mapping.

Abstract

submitted to Experimental Astronomy, Special Issue for Cosmic Vision 2007

Abstract

International audience

Additional details

Created:
December 4, 2022
Modified:
November 30, 2023