dc.contributor.author
Jones, Geraint H.
dc.contributor.author
Snodgrass, Colin
dc.contributor.author
Tubiana, Cecilia
dc.contributor.author
Küppers, Michael
dc.contributor.author
Kawakita, Hideyo
dc.contributor.author
Lara, Luisa M.
dc.contributor.author
Agarwal, Jessica
dc.contributor.author
André, Nicolas
dc.contributor.author
Attree, Nicholas
dc.contributor.author
Postberg, Frank
dc.date.accessioned
2024-06-26T06:34:50Z
dc.date.available
2024-06-26T06:34:50Z
dc.identifier.uri
https://refubium.fu-berlin.de/handle/fub188/43979
dc.identifier.uri
http://dx.doi.org/10.17169/refubium-43688
dc.description.abstract
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 Delta 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.
en
dc.format.extent
83 Seiten
dc.rights.uri
https://creativecommons.org/licenses/by/4.0/
dc.subject
Instruments – spaceborne and space research
en
dc.subject.ddc
500 Naturwissenschaften und Mathematik::520 Astronomie::520 Astronomie und zugeordnete Wissenschaften
dc.title
The Comet Interceptor Mission
dc.type
Wissenschaftlicher Artikel
dcterms.bibliographicCitation.articlenumber
9
dcterms.bibliographicCitation.doi
10.1007/s11214-023-01035-0
dcterms.bibliographicCitation.journaltitle
Space Science Reviews
dcterms.bibliographicCitation.number
1
dcterms.bibliographicCitation.volume
220
dcterms.bibliographicCitation.url
https://doi.org/10.1007/s11214-023-01035-0
refubium.affiliation
Geowissenschaften
refubium.affiliation.other
Institut für Geologische Wissenschaften / Fachrichtung Planetologie und Fernerkundung

refubium.resourceType.isindependentpub
no
dcterms.accessRights.openaire
open access
dcterms.isPartOf.eissn
1572-9672
refubium.resourceType.provider
WoS-Alert