Journal
PLANETARY AND SPACE SCIENCE
Volume 225, Issue -, Pages -Publisher
PERGAMON-ELSEVIER SCIENCE LTD
DOI: 10.1016/j.pss.2022.105610
Keywords
Trojan; Mission; Analysis; Jupiter; Swingby; In -situ
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The NASA mission Lucy, launched in 2021, will flyby several Jupiter Trojan asteroids. The next step is to design a mission with a close orbiter and/or lander for in situ science at specific Trojans. This paper presents a feasible design for such a mission to the largest Jupiter Trojan, 624 Hektor, and finds that the suggested principle can be applied to other target Trojans as well.
The NASA mission Lucy, launched in 2021, will perform flybys at several Jupiter Trojan asteroids. The logical next step is a close orbiter and/or lander for in situ science at specific Trojans. The present paper reports results for a feasible design of such a mission to the largest Jupiter Trojan, 624 Hektor. The suggested principle, which involves a powered Jupiter gravity assist followed by an extended drift arc towards the target body and an insertion maneuver of around 1 km/s, has been found to lead to comparable mission options for a number of other target Trojans.
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