Articolo in rivista, 2021, ENG, 10.1016/j.actaastro.2020.12.045
F. Salazar, A. Alkhaja, E. Fantino, E.M. Alessi
Department of Aerospace Engineering, Khalifa University of Science and Technology, Abu Dhabi (UAE); IMATI-CNR; IFAC-CNR
This contribution investigates the properties of a category of orbits around Enceladus. The motivation is the interest in the in situ exploration of this moon following Cassini's detection of plumes of water and organic compounds close to its south pole. In a previous investigation, a set of heteroclinic connections were designed between halo orbits around the equilibrium points L1 and L2 of the circular restricted three-body problem with Saturn and Enceladus as primaries. The kinematical and geometrical characteristics of those trajectories makes them good candidates as science orbits for the extended observation of the surface of Enceladus: they are highly inclined, they approach the moon and they are maneuver-free. However, the low heights above the surface and the strong perturbing effect of Saturn impose a more careful look at their dynamics, in particular regarding the influence of the polar flattening of the primaries. Therefore, those solutions are here reconsidered by employing a dynamical model that includes the effect of the oblateness of Saturn and Enceladus, individually and in combination. The dynamical equivalents of the halo orbits around the equilibrium points L1 and L2 and their stable and unstable hyperbolic invariant manifolds are obtained in the perturbed models, and maneuver-free heteroclinic connections are identified in the new framework. A systematic comparison with the corresponding solutions of the unperturbed problem shows that qualitative and quantitative features are not significantly altered when the oblateness of the primaries is taken into account. Further- more, it is found that the J2 coefficient of Saturn plays a larger role than that of Enceladus. From a mission perspective, the results confirm the scientific value of the solutions obtained in the classical circular restricted threebody problem and suggests that this simpler model can be used in a preliminary feasibility analysis.
Acta astronautica 180 , pp. 398–416
Circular Restricted Three-Body Problem, Saturn, Enceladus, First zonal harmonic coefficient, Libration Point Orbits, Heteroclinic connections, Science orbits
IFAC – Istituto di fisica applicata "Nello Carrara", IMATI – Istituto di matematica applicata e tecnologie informatiche "Enrico Magenes"
ID: 440352
Year: 2021
Type: Articolo in rivista
Creation: 2020-12-27 15:38:05.000
Last update: 2021-03-25 16:16:58.000
CNR authors
External links
OAI-PMH: Dublin Core
OAI-PMH: Mods
OAI-PMH: RDF
DOI: 10.1016/j.actaastro.2020.12.045
URL: https://www.sciencedirect.com/science/article/abs/pii/S0094576520307876?via%3Dihub
External IDs
CNR OAI-PMH: oai:it.cnr:prodotti:440352
DOI: 10.1016/j.actaastro.2020.12.045
ISI Web of Science (WOS): 000613150200041
Scopus: 2-s2.0-85099006554