ESA F-Class Comet Interceptor: Trajectory Design to Intercept a Yet-to-be-discovered Comet
Joan Pau S\'anchez, David Morante, Pablo Hermosin, Daniel Ranuschio,, Alvaro Estalella, Dayana Viera, Simone Centuori, Geraint Jones, Colin, Snodgrass, Anny Chantal Levasseur-Regourd, Cecilia Tubiana

TL;DR
The paper discusses the trajectory design and mission planning for ESA's Comet Interceptor to intercept yet-to-be-discovered long-period comets, analyzing target accessibility, transfer options, and success probabilities.
Contribution
It introduces a comprehensive trajectory analysis for a mission targeting unknown comets, including propulsion trade-offs and probabilistic success assessment.
Findings
2-3 feasible targets expected annually
Lunar swing-by enhances Earth escape options
95-99% success probability within 6 years
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…
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