ESA F-Class Comet Interceptor: trajectory design to intercept a yet-to-be-discovered comet
dc.contributor.author | Sánchez, Joan-Pau | |
dc.contributor.author | Morante, David | |
dc.contributor.author | Hermosin, Pablo | |
dc.contributor.author | Ranuschio, Daniel | |
dc.contributor.author | Estalella, Alvaro | |
dc.contributor.author | Viera, Dayana | |
dc.contributor.author | Centuori, Simone | |
dc.contributor.author | Jones, Geraint | |
dc.contributor.author | Snodgrass, Colin | |
dc.contributor.author | Levasseur-Regourd, Anny Chantal | |
dc.contributor.author | Tubiana, Cecilia | |
dc.date.accessioned | 2021-07-21T15:00:39Z | |
dc.date.available | 2021-07-21T15:00:39Z | |
dc.date.issued | 2021-07-16 | |
dc.description.abstract | Comet Interceptor (Comet-I) was selected in June 2019 as the first ESA F-Class mission. In 2029+, Comet-I will hitch a ride to a Sun-Earth L2 quasi-halo orbit, as a co-passenger of ESA's M4 ARIEL mission. It will then remain idle at the L2 point until the right departure conditions are met to intercept a yet-to-be-discovered long period comet (or interstellar body). The fact that Comet-I target is thus unidentified becomes a key aspect of the trajectory and mission design. The paper first analyses the long period comet population and concludes that 2 to 3 feasible targets a year should be expected. Yet, Comet-I will only be able to access some of these, depending mostly on the angular distance between the Earth and the closest nodal point to the Earth's orbit radius. A preliminary analysis of the transfer trajectories has been performed to assess the trade-off between the accessible region and the transfer time for a given spacecraft design, including a fully chemical, a fully electric and a hybrid propulsion system. The different Earth escape options also play a paramount role to enhance Comet-I capability to reach possible long period comet targets. Particularly, Earth-leading intercept configurations have the potential to benefit the most from lunar swing-by departures. Finally, a preliminary Monte Carlo analysis shows that Comet-I has a 95–99% likelihood of successfully visit a pristine newly-discovered long period comet in less than 6 years of mission timespan. | en_UK |
dc.identifier.citation | Sánchez JP, Morante D, Hermosin P, et al., (2021) ESA F-Class Comet Interceptor: trajectory design to intercept a yet-to-be-discovered comet. Acta Astronautica, Volume 188, November 2021, pp. 265-277 | en_UK |
dc.identifier.issn | 0094-5765 | |
dc.identifier.uri | https://doi.org/10.1016/j.actaastro.2021.07.014 | |
dc.identifier.uri | https://dspace.lib.cranfield.ac.uk/handle/1826/16912 | |
dc.language.iso | en | en_UK |
dc.publisher | Elsevier | en_UK |
dc.rights | Attribution-NonCommercial-NoDerivatives 4.0 International | * |
dc.rights.uri | http://creativecommons.org/licenses/by-nc-nd/4.0/ | * |
dc.subject | Lunar swing-by | en_UK |
dc.subject | Third body effects | en_UK |
dc.subject | Hybrid propulsion trajectories | en_UK |
dc.subject | Trajectory design | en_UK |
dc.subject | Comet-I | en_UK |
dc.title | ESA F-Class Comet Interceptor: trajectory design to intercept a yet-to-be-discovered comet | en_UK |
dc.type | Article | en_UK |
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