Issue |
A&A
Volume 642, October 2020
The Solar Orbiter mission
|
|
---|---|---|
Article Number | A9 | |
Number of page(s) | 11 | |
Section | Astronomical instrumentation | |
DOI | https://doi.org/10.1051/0004-6361/201937257 | |
Published online | 30 September 2020 |
The Solar Orbiter magnetometer
1
Imperial College London, South Kensington Campus, London SW7 2AZ, UK
e-mail: t.horbury@imperial.ac.uk
2
Evonetix Ltd, Cambridge, UK
3
Arquimea Ingenieria, Madrid, Spain
4
Atomio, Lille, France
5
CERN, Geneva, Switzerland
6
Mullard Space Science Laboratory, University College London, Holmbury St. Mary, UK
7
School of Physics and Astronomy, Queen Mary University of London, London E1 4NS, UK
8
SUPA School of Physics and Astronomy, University of Glasgow, Glasgow G12 8QQ, UK
9
Univ. Reading, Dept. Meteorol., Reading RG6 6BB, Berks, UK
10
Centre for Fusion, Space & Astrophysics, Physics Dept., University of Warwick, Coventry, UK
11
Jeremiah Horrocks Institute, University of Central Lancashire, Preston, UK
12
Space Sciences Laboratory, University of California, Berkeley, CA 94720-7450, USA
13
Space Research Institute, Austrian Academy of Sciences, Graz, Austria
14
University of Calabria, Dipartimento Fis, Arcavacata di Rende, Cosenza, Italy
15
Wigner RCP, Budapest, Hungary
16
Lunar and Planetary Laboratory, U. Arizona, Tucson, AZ, USA
17
Technical University of Braunschweig, IGEP, Mendelssohnstr. 3, Braunschweig, Germany
18
University of Maryland Baltimore County, Goddard Planetary Heliophys Inst., Baltimore, MD, USA
19
Stanford University, Stanford, CA, USA
20
LESIA, Observatoire de Paris, Universite PSL, CNRS, Sorbonne Universite, Universite de Paris, 5 Pl. Jules Janssen, 92190 Meudon, France
21
Institut für Experimentelle und Angewandte Physik, Christian-Albrechts-Universität zu Kiel, Kiel, Germany
22
University of Delaware, Newark, DE, USA
23
Universidad de Alcala, Madrid, Spain
24
NASA Jet Propulsion Laboratory, Pasadena, USA
25
Predictive Science Inc., San Diego, CA, USA
26
University of California Los Angeles, Inst. Geophys. & Planetary Phys., Dept. Earth Planetary & Space Sci., Los Angeles, CA, USA
27
University of Turku, Dept. Phys. & Astron., Turku, Finland
28
Technical University of Denmark, Natl. Space Inst., Copenhagen, Denmark
29
Center for Space and Aeronomic Research (CSPAR) and Department of Space Science, University of Alabama in Huntsville, Huntsville, USA
30
European Space Agency, ESTEC (SCI-S), PO Box 299, Noordwijk 2200 AG, The Netherlands
31
European Space Agency, ESAC (SCI-S), Madrid, Spain
32
University of Colorado, Boulder, CO, USA
33
Physics Department, University of California, Berkeley, CA 94720-7300, USA
Received:
4
December
2019
Accepted:
27
January
2020
The magnetometer instrument on the Solar Orbiter mission is designed to measure the magnetic field local to the spacecraft continuously for the entire mission duration. The need to characterise not only the background magnetic field but also its variations on scales from far above to well below the proton gyroscale result in challenging requirements on stability, precision, and noise, as well as magnetic and operational limitations on both the spacecraft and other instruments. The challenging vibration and thermal environment has led to significant development of the mechanical sensor design. The overall instrument design, performance, data products, and operational strategy are described.
Key words: space vehicles: instruments / solar wind / Sun: magnetic fields / Sun: heliosphere
© ESO 2020
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