TY - JOUR
T1 - The Comet Interceptor Mission
AU - Jones, Geraint H.
AU - Snodgrass, Colin
AU - Tubiana, Cecilia
AU - Küppers, Michael
AU - Kawakita, Hideyo
AU - Lara, Luisa M.
AU - Agarwal, Jessica
AU - André, Nicolas
AU - Attree, Nicholas
AU - Auster, Uli
AU - Bagnulo, Stefano
AU - Bannister, Michele
AU - Beth, Arnaud
AU - Bowles, Neil
AU - Coates, Andrew
AU - Colangeli, Luigi
AU - Corral van Damme, Carlos
AU - Da Deppo, Vania
AU - De Keyser, Johan
AU - Della Corte, Vincenzo
AU - Edberg, Niklas
AU - El-Maarry, Mohamed Ramy
AU - Faggi, Sara
AU - Fulle, Marco
AU - Funase, Ryu
AU - Galand, Marina
AU - Goetz, Charlotte
AU - Groussin, Olivier
AU - Guilbert-Lepoutre, Aurélie
AU - Henri, Pierre
AU - Kasahara, Satoshi
AU - Kereszturi, Akos
AU - Kidger, Mark
AU - Knight, Matthew
AU - Kokotanekova, Rosita
AU - Kolmasova, Ivana
AU - Kossacki, Konrad
AU - Kührt, Ekkehard
AU - Kwon, Yuna
AU - La Forgia, Fiorangela
AU - Levasseur-Regourd, Anny Chantal
AU - Lippi, Manuela
AU - Longobardo, Andrea
AU - Marschall, Raphael
AU - Morawski, Marek
AU - Muñoz, Olga
AU - Näsilä, Antti
AU - Nilsson, Hans
AU - Opitom, Cyrielle
AU - Pajusalu, Mihkel
N1 - Publisher Copyright:
© 2024, The Author(s).
PY - 2024/2
Y1 - 2024/2
N2 - Here we describe the novel, multi-point Comet Interceptor mission. It is dedicated to the exploration of a little-processed long-period comet, possibly entering the inner Solar System for the first time, or to encounter an interstellar object originating at another star. The objectives of the mission are to address the following questions: What are the surface composition, shape, morphology, and structure of the target object? What is the composition of the gas and dust in the coma, its connection to the nucleus, and the nature of its interaction with the solar wind? The mission was proposed to the European Space Agency in 2018, and formally adopted by the agency in June 2022, for launch in 2029 together with the Ariel mission. Comet Interceptor will take advantage of the opportunity presented by ESA’s F-Class call for fast, flexible, low-cost missions to which it was proposed. The call required a launch to a halo orbit around the Sun-Earth L2 point. The mission can take advantage of this placement to wait for the discovery of a suitable comet reachable with its minimum Δ V capability of 600 ms − 1 . Comet Interceptor will be unique in encountering and studying, at a nominal closest approach distance of 1000 km, a comet that represents a near-pristine sample of material from the formation of the Solar System. It will also add a capability that no previous cometary mission has had, which is to deploy two sub-probes – B1, provided by the Japanese space agency, JAXA, and B2 – that will follow different trajectories through the coma. While the main probe passes at a nominal 1000 km distance, probes B1 and B2 will follow different chords through the coma at distances of 850 km and 400 km, respectively. The result will be unique, simultaneous, spatially resolved information of the 3-dimensional properties of the target comet and its interaction with the space environment. We present the mission’s science background leading to these objectives, as well as an overview of the scientific instruments, mission design, and schedule.
AB - Here we describe the novel, multi-point Comet Interceptor mission. It is dedicated to the exploration of a little-processed long-period comet, possibly entering the inner Solar System for the first time, or to encounter an interstellar object originating at another star. The objectives of the mission are to address the following questions: What are the surface composition, shape, morphology, and structure of the target object? What is the composition of the gas and dust in the coma, its connection to the nucleus, and the nature of its interaction with the solar wind? The mission was proposed to the European Space Agency in 2018, and formally adopted by the agency in June 2022, for launch in 2029 together with the Ariel mission. Comet Interceptor will take advantage of the opportunity presented by ESA’s F-Class call for fast, flexible, low-cost missions to which it was proposed. The call required a launch to a halo orbit around the Sun-Earth L2 point. The mission can take advantage of this placement to wait for the discovery of a suitable comet reachable with its minimum Δ V capability of 600 ms − 1 . Comet Interceptor will be unique in encountering and studying, at a nominal closest approach distance of 1000 km, a comet that represents a near-pristine sample of material from the formation of the Solar System. It will also add a capability that no previous cometary mission has had, which is to deploy two sub-probes – B1, provided by the Japanese space agency, JAXA, and B2 – that will follow different trajectories through the coma. While the main probe passes at a nominal 1000 km distance, probes B1 and B2 will follow different chords through the coma at distances of 850 km and 400 km, respectively. The result will be unique, simultaneous, spatially resolved information of the 3-dimensional properties of the target comet and its interaction with the space environment. We present the mission’s science background leading to these objectives, as well as an overview of the scientific instruments, mission design, and schedule.
KW - Comets
KW - Instruments – spaceborne and space research
KW - Spacecraft
UR - https://www.scopus.com/pages/publications/85183417097
U2 - 10.1007/s11214-023-01035-0
DO - 10.1007/s11214-023-01035-0
M3 - Article
AN - SCOPUS:85183417097
SN - 0038-6308
VL - 220
JO - Space Science Reviews
JF - Space Science Reviews
IS - 1
M1 - 9
ER -