The Solar Orbiter magnetometer

被引：209

作者：

Horbury, T. S. ^{[1
]}

O'Brien, H. ^{[1
]}

Blazquez, I. Carrasco ^{[1
]}

Bendyk, M. ^{[1
]}

Brown, P. ^{[1
]}

Hudson, R. ^{[1
]}

Evans, V. ^{[1
]}

Oddy, T. M. ^{[1
]}

Carr, C. M. ^{[1
]}

Beek, T. J. ^{[1
]}

Cupido, E. ^{[1
]}

Bhattacharya, S. ^{[2
]}

Dominguez, J. -A. ^{[3
]}

Matthews, L. ^{[4
]}

Myklebust, V. R. ^{[5
]}

Whiteside, B. ^{[6
]}

Bale, S. D. ^{[12
,34
]}

Baumjohann, W. ^{[13
]}

Burgess, D. ^{[7
]}

Carbone, V. ^{[14
]}

Cargill, P. ^{[1
]}

Eastwood, J. ^{[1
]}

Erdos, G. ^{[15
]}

Fletcher, L. ^{[8
]}

Forsyth, R. ^{[1
]}

Giacalone, J. ^{[16
]}

Glassmeier, K. -H. ^{[17
]}

Goldstein, M. L. ^{[18
]}

Hoeksema, T. ^{[19
]}

Lockwood, M. ^{[9
]}

Magnes, W. ^{[13
]}

Maksimovic, M. ^{[20
]}

Marsch, E. ^{[21
]}

Matthaeus, W. H. ^{[22
]}

Murphy, N. ^{[24
]}

Nakariakov, V. M. ^{[10
]}

Owen, C. J. ^{[6
]}

Owens, M. ^{[9
]}

Rodriguez-Pacheco, J. ^{[23
]}

Richter, I. ^{[17
]}

Riley, P. ^{[25
]}

Russell, C. T. ^{[26
]}

Schwartz, S. ^{[33
]}

Vainio, R. ^{[27
]}

Velli, M. ^{[26
]}

Vennerstrom, S. ^{[28
]}

Walsh, R. ^{[11
]}

Wimmer-Schweingruber, R. F. ^{[21
]}

Zank, G. ^{[29
,30
]}

Muller, D. ^{[31
]}

机构：

[1] Imperial Coll London, South Kensington Campus, London SW7 2AZ, England

[2] Evonetix Ltd, Cambridge, England

[3] Arquimea Ingn, Madrid, Spain

[4] Atomio, Lille, France

[5] CERN, Geneva, Switzerland

[6] UCL, Mullard Space Sci Lab, Holmbury St Mary, London, England

[7] Queen Mary Univ London, Sch Phys & Astron, London E1 4NS, England

[8] Univ Glasgow, SUPA Sch Phys & Astron, Glasgow G12 8QQ, Lanark, Scotland

[9] Univ Reading, Dept Meteorol, Reading RG6 6BB, Berks, England

[10] Univ Warwick, Ctr Fus Space & Astrophys, Phys Dept, Coventry, W Midlands, England

[11] Univ Cent Lancashire, Jeremiah Horrocks Inst, Preston, Lancs, England

[12] Univ Calif Berkeley, Space Sci Lab, Berkeley, CA 94720 USA

[13] Austrian Acad Sci, Space Res Inst, Graz, Austria

[14] Univ Calabria, Dipartimento Fis, Arcavacata Di Rende, Cosenza, Italy

[15] Wigner RCP, Budapest, Hungary

[16] Univ Arizona, Lunar & Planetary Lab, Tucson, AZ 85721 USA

[17] Tech Univ Carolo Wilhelmina Braunschweig, IGEP, Mendelssohnstr 3, Braunschweig, Germany

[18] Univ Maryland Baltimore Cty, Goddard Planetary Heliophys Inst, Baltimore, MD 21228 USA

[19] Stanford Univ, Stanford, CA USA

[20] Univ Paris, Univ PSL, Sorbonne Univ, LESIA,Observ Paris,CNRS, 5 Pl Jules Janssen, F-92190 Meudon, France

[21] Christian Albrechts Univ Kiel, Inst Expt & Angew Phys, Kiel, Germany

[22] Univ Delaware, Newark, DE USA

[23] Univ Alcala, Madrid, Spain

[24] NASA, Jet Prop Lab, Pasadena, CA USA

[25] Predict Sci Inc, San Diego, CA USA

[26] Univ Calif Los Angeles, Inst Geophys & Planetary Phys, Dept Earth Planetary & Space Sci, Los Angeles, CA 90024 USA

[27] Univ Turku, Dept Phys & Astron, Turku, Finland

[28] Tech Univ Denmark, Natl Space Inst, Copenhagen, Denmark

[29] Univ Alabama, Ctr Space & Aeron Res CSPAR, Huntsville, AL 35899 USA

[30] Univ Alabama, Dept Space Sci, Huntsville, AL 35899 USA

[31] ESTEC SCI S, European Space Agcy, POB 299, NL-2200 AG Noordwijk, Netherlands

[32] ESAC SCI S, European Space Agcy, Madrid, Spain

[33] Univ Colorado, Boulder, CO 80309 USA

[34] Univ Calif Berkeley, Dept Phys, Berkeley, CA 94720 USA

来源：

ASTRONOMY & ASTROPHYSICS | 2020年 / 642卷

基金：

英国科学技术设施理事会;

关键词：

space vehicles: instruments; solar wind; Sun: magnetic fields; Sun: heliosphere; COROTATING INTERACTION REGIONS; WIND; SUN; HELIOSPHERE; SCIENCE; SPACE;

D O I：

10.1051/0004-6361/201937257

中图分类号：

P1 [天文学];

学科分类号：

0704 ;

摘要：

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.

引用

页数：11

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