The work study the landing of a spacecraft on the Jupiter satellite Callisto with minimal energy costs, and the minimum required thrust of the engines and the duration of the soft landing maneuver of a spacecraft with a given mass on the satellite were estimated. A distinctive feature of this study is taking into account the weak atmosphere of Callisto, which, however, in the immediate vicinity of the surface has a noticeable aerodynamic drag. Motion modeling was carried out numerically; all the graphical dependencies necessary for motion analysis were built.
Spacecraft Control During The Descent to The Surface of Jupiter's Satellite Callisto
07.06.2023
467137 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Ballistic analysis of a mission to Jupiter’s moon Callisto with landing on the surface
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