Phd in AERONAUTICS AND SPACE ENGINEERING

Thesis title: Gravitational Gradiometry for Planetary Missions

The measurement of the gravitational field of Solar System bodies is increasingly becoming crucial in the physical description of their composition, state and evolution. Gravity field measurements are one of the observational methods to investigate those topics and to place constraints on the structure of the planetary interiors, the formation and geologic evolution of a planet. The retrieval of the spherical harmonic coefficients used to describe the gravitational field of a body gives insights into e.g. its polar oblateness, moment of inertia and deviations from hydrostatic equilibrium. With geologic assumptions and other remote sensing data, significant geophysical parameters, related e.g. to crust and mantle density and thickness, core size and structure, mantle/core coupling can be obtained. These parameters are used in planetary models to address topics such as planets differentiation, thermal evolution, characteristics and composition of the interiors. Until now, the Radio-Tracking technique (RT), part of the Radio Science (RS) observations, jointly with POD (Precise Orbit Determination), has been de-facto the main technique for gathering this type of information. It has been implemented in several deep-space missions, such as Magellan (Venus), MRO (Mars), Cassini (Saturn), Messenger (Mercury), Juno (Jupiter), and, in the forthcoming future, BepiColombo (Mercury) and JUICE (Jupiter and its moons). Concerning scientific targets of interest, it needs to be highlighted that gravity field models are available, besides the Earth and the Moon, just for few planetary bodies such as the terrestrial planets Mercury, Venus and Mars. However, often such models are restricted only to large spatial resolutions, about one or more hundreds of kilometers, not enough to understand the geophysical processes that have driven formation and evolution of those bodies; the accuracy of these models is good enough as well but just for the lower part of the gravity field spectra, where a sufficient signal-to-noise ratio is achieved. Moreover, there is much more lack of data for the external planets, where only few gravity field parameters have been derived for some of the gaseous planets and their main moons. To answer the need for higher space resolution and accuracy in planetary gravity fields, two different approaches can be pursued: 1. to improve the measurement performance of the instrumentation used for RS; 2. to define innovative measurement concepts, allowing to overcome some of the bottlenecks of the current methods (non-continuous monitoring, field attenuation with the altitude, disturbances mitigation, etc.,). In a roadmap definition, one of the more promising is the gravity gradiometry technique, which would allow to directly sense the gravity field by measuring the gravity gradients, and not just indirectly, as for RT, through monitoring the spacecraft gravitational perturbations. Unlike the radio-tracking, space-based gravity gradiometry has still to unfold its potentialities; indeed, the ESA’s GOCE mission is the first and unique till now that has flown a gravity gradiometer to explore Earth’s gravity in 2009-13. The planetary gradiometry still awaits achievements outside the Earth System. Satellite gradiometry is the measurement of acceleration differences, ideally in all three spatial directions, between the test-masses of an ensemble of accelerometers inside one satellite. The differentiation of gravity accelerations allows to highlight small-scale surface and sub-surface features, making such a technique, differently wrt RT, inherently sensitive to medium and large degrees (i.e. high resolutions) of the spherical harmonic representation of the gravity field. Therefore, the use of gradiometry would allow to improve the gravity field knowledge by measuring medium and large degrees, filling the gap above depicted and fostering the investigation on the structure and evolution of the planets. The activity of this PhD Thesis foresees the definition of the planetary gravity field state of the art and the identification of the needs of the scientific community to improve the planetary bodies knowledge. Based on this result, a selection of targets of interest has been operated. A review of the gravity field measurement techniques has been carried out, identifying advantages and drawbacks, pointing out innovative techniques such as gradiometry. On the basis of these activities, a series of numerical simulations has been implemented to produce the time series of gradiometric signals foreseen in a set of case studies. The choice of the case studies was based on the preliminary studies about the science needs. The main outcome was a set of requirements to be matched by a typical gradiometric instrument/mission, aiming at fulfilling the scientific needs. An important requirement is, for instance, the typical instrument sensitivity and spectral band, as well as the expected acceleration or gravity gradient amplitude of a signal sensed with a reasonable signal-to-noise ratio. Different scenarios were simulated on the basis of the science needs. In chapter 2 the gravity field is faced from the theoretical point of view and a snapshot of the current understanding of gravity field of planetary bodies is carried out. At last, science needs are identified and planetary bodies of interest are selected. In chapter 3 measurement techniques of the gravity field are described, focusing the attention on the gravitational gradiometry. Advantages and drawbacks are considered. Moreover, spaceborne, airborne and groundborne gradiometric instruments have been identified and analysed to identify the current state of the art. In chapter 4 science needs are compared to the instruments status. Afterwards, a matlab code to compute the gravity gradient signal expected in some case studies is described and evaluated. In chapter 5 a hyphotesis of cross-component gradiometer is analysed and basic performance are derived and compared to the signal that is expected to be measured according to the computation carried out with the matlab code. Moreover, the needs of a gravity mission are faced. Further development and analysis of gradiometer configurations is considered as future work.