CARIOQA: Definition of a Quantum Pathfinder Mission

Publikation: Beitrag in Buch/Bericht/Sammelwerk/KonferenzbandAufsatz in KonferenzbandForschungPeer-Review

Autoren

  • T. Lévèque
  • C. Fallet
  • J. Lefebve
  • A. Piquereau
  • A. Gauguet
  • B. Battelier
  • P. Bouyer
  • N. Gaaloul
  • M. Lachmann
  • B. Piest
  • E. Rasel
  • J. Müller
  • C. Schubert
  • Q. Beaufils
  • F. Pereira Dos Santos

Organisationseinheiten

Externe Organisationen

  • Centre national d’études spatiales (CNES)
  • Université Toulouse III – Paul Sabatier (UT3)
  • Universite de Bordeaux
  • Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)
  • Observatoire de Paris (OBSPARIS)
Forschungs-netzwerk anzeigen

Details

OriginalspracheEnglisch
Titel des SammelwerksInternational Conference on Space Optics, ICSO 2022
Herausgeber/-innenKyriaki Minoglou, Nikos Karafolas, Bruno Cugny
Herausgeber (Verlag)SPIE
ISBN (elektronisch)9781510668034
PublikationsstatusVeröffentlicht - 12 Juli 2023
Veranstaltung2022 International Conference on Space Optics, ICSO 2022 - Dubrovnik, Kroatien
Dauer: 3 Okt. 20227 Okt. 2022

Publikationsreihe

NameProceedings of SPIE - The International Society for Optical Engineering
Band12777
ISSN (Print)0277-786X
ISSN (elektronisch)1996-756X

Abstract

A strong potential gain for space applications is expected from the anticipated performances of inertial sensors based on cold atom interferometry (CAI) that measure the acceleration of freely falling independent atoms by manipulating them with laser light. In this context, CNES and its partners initiated a phase 0 study, called CARIOQA, in order to develop a Quantum Pathfinder Mission unlocking key features of atom interferometry for space and paving the way for future ambitious space missions utilizing this technology. As a cornerstone for the implementation of quantum sensors in space, the CARIOQA phase 0 aimed at defining the Quantum Pathfinder Mission's scenario and associated performance objectives. To comply with these objectives, the payload architecture has been designed to achieve long interrogation time and active rotation compensation on a BEC-based atom interferometer. A study of the satellite architecture, including all the subsystems, has been conducted. Several technical solutions for propulsion and attitude control have been investigated in order to guarantee optimal operating conditions (limitation of micro-vibrations, maximization of measurement time). A preliminary design of the satellite platform was performed.

ASJC Scopus Sachgebiete

Zitieren

CARIOQA: Definition of a Quantum Pathfinder Mission. / Lévèque, T.; Fallet, C.; Lefebve, J. et al.
International Conference on Space Optics, ICSO 2022. Hrsg. / Kyriaki Minoglou; Nikos Karafolas; Bruno Cugny. SPIE, 2023. 127773L (Proceedings of SPIE - The International Society for Optical Engineering; Band 12777).

Publikation: Beitrag in Buch/Bericht/Sammelwerk/KonferenzbandAufsatz in KonferenzbandForschungPeer-Review

Lévèque, T, Fallet, C, Lefebve, J, Piquereau, A, Gauguet, A, Battelier, B, Bouyer, P, Gaaloul, N, Lachmann, M, Piest, B, Rasel, E, Müller, J, Schubert, C, Beaufils, Q & Dos Santos, FP 2023, CARIOQA: Definition of a Quantum Pathfinder Mission. in K Minoglou, N Karafolas & B Cugny (Hrsg.), International Conference on Space Optics, ICSO 2022., 127773L, Proceedings of SPIE - The International Society for Optical Engineering, Bd. 12777, SPIE, 2022 International Conference on Space Optics, ICSO 2022, Dubrovnik, Kroatien, 3 Okt. 2022. https://doi.org/10.48550/arXiv.2211.01215, https://doi.org/10.1117/12.2690536
Lévèque, T., Fallet, C., Lefebve, J., Piquereau, A., Gauguet, A., Battelier, B., Bouyer, P., Gaaloul, N., Lachmann, M., Piest, B., Rasel, E., Müller, J., Schubert, C., Beaufils, Q., & Dos Santos, F. P. (2023). CARIOQA: Definition of a Quantum Pathfinder Mission. In K. Minoglou, N. Karafolas, & B. Cugny (Hrsg.), International Conference on Space Optics, ICSO 2022 Artikel 127773L (Proceedings of SPIE - The International Society for Optical Engineering; Band 12777). SPIE. https://doi.org/10.48550/arXiv.2211.01215, https://doi.org/10.1117/12.2690536
Lévèque T, Fallet C, Lefebve J, Piquereau A, Gauguet A, Battelier B et al. CARIOQA: Definition of a Quantum Pathfinder Mission. in Minoglou K, Karafolas N, Cugny B, Hrsg., International Conference on Space Optics, ICSO 2022. SPIE. 2023. 127773L. (Proceedings of SPIE - The International Society for Optical Engineering). doi: 10.48550/arXiv.2211.01215, 10.1117/12.2690536
Lévèque, T. ; Fallet, C. ; Lefebve, J. et al. / CARIOQA : Definition of a Quantum Pathfinder Mission. International Conference on Space Optics, ICSO 2022. Hrsg. / Kyriaki Minoglou ; Nikos Karafolas ; Bruno Cugny. SPIE, 2023. (Proceedings of SPIE - The International Society for Optical Engineering).
Download
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abstract = "A strong potential gain for space applications is expected from the anticipated performances of inertial sensors based on cold atom interferometry (CAI) that measure the acceleration of freely falling independent atoms by manipulating them with laser light. In this context, CNES and its partners initiated a phase 0 study, called CARIOQA, in order to develop a Quantum Pathfinder Mission unlocking key features of atom interferometry for space and paving the way for future ambitious space missions utilizing this technology. As a cornerstone for the implementation of quantum sensors in space, the CARIOQA phase 0 aimed at defining the Quantum Pathfinder Mission's scenario and associated performance objectives. To comply with these objectives, the payload architecture has been designed to achieve long interrogation time and active rotation compensation on a BEC-based atom interferometer. A study of the satellite architecture, including all the subsystems, has been conducted. Several technical solutions for propulsion and attitude control have been investigated in order to guarantee optimal operating conditions (limitation of micro-vibrations, maximization of measurement time). A preliminary design of the satellite platform was performed.",
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AU - Piquereau, A.

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AU - Battelier, B.

AU - Bouyer, P.

AU - Gaaloul, N.

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N2 - A strong potential gain for space applications is expected from the anticipated performances of inertial sensors based on cold atom interferometry (CAI) that measure the acceleration of freely falling independent atoms by manipulating them with laser light. In this context, CNES and its partners initiated a phase 0 study, called CARIOQA, in order to develop a Quantum Pathfinder Mission unlocking key features of atom interferometry for space and paving the way for future ambitious space missions utilizing this technology. As a cornerstone for the implementation of quantum sensors in space, the CARIOQA phase 0 aimed at defining the Quantum Pathfinder Mission's scenario and associated performance objectives. To comply with these objectives, the payload architecture has been designed to achieve long interrogation time and active rotation compensation on a BEC-based atom interferometer. A study of the satellite architecture, including all the subsystems, has been conducted. Several technical solutions for propulsion and attitude control have been investigated in order to guarantee optimal operating conditions (limitation of micro-vibrations, maximization of measurement time). A preliminary design of the satellite platform was performed.

AB - A strong potential gain for space applications is expected from the anticipated performances of inertial sensors based on cold atom interferometry (CAI) that measure the acceleration of freely falling independent atoms by manipulating them with laser light. In this context, CNES and its partners initiated a phase 0 study, called CARIOQA, in order to develop a Quantum Pathfinder Mission unlocking key features of atom interferometry for space and paving the way for future ambitious space missions utilizing this technology. As a cornerstone for the implementation of quantum sensors in space, the CARIOQA phase 0 aimed at defining the Quantum Pathfinder Mission's scenario and associated performance objectives. To comply with these objectives, the payload architecture has been designed to achieve long interrogation time and active rotation compensation on a BEC-based atom interferometer. A study of the satellite architecture, including all the subsystems, has been conducted. Several technical solutions for propulsion and attitude control have been investigated in order to guarantee optimal operating conditions (limitation of micro-vibrations, maximization of measurement time). A preliminary design of the satellite platform was performed.

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ER -

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