A1 Vertaisarvioitu alkuperäisartikkeli tieteellisessä lehdessä
The Solar Orbiter magnetometer
Tekijät: Horbury TS, O'Brien H, Blazquez IC, Bendyk M, Brown P, Hudson R, Evans V, Oddy TM, Carr CM, Beek TJ, Cupido E, Bhattacharya S, Dominguez JA, Matthews L, Myklebust VR, Whiteside B, Bale SD, Baumjohann W, Burgess D, Carbone V, Cargill P, Eastwood J, Erdos G, Fletcher L, Forsyth R, Giacalone J, Glassmeier KH, Goldstein ML, Hoeksema T, Lockwood M, Magnes W, Maksimovic M, Marsch E, Matthaeus WH, Murphy N, Nakariakov VM, Owen CJ, Owens M, Rodriguez-Pacheco J, Richter I, Riley P, Russell CT, Schwartz S, Vainio R, Velli M, Vennerstrom S, Walsh R, Wimmer-Schweingruber RF, Zank G, Muller D, Zouganelis I, Walsh AP
Kustantaja: EDP SCIENCES S A
Julkaisuvuosi: 2020
Journal: Astronomy and Astrophysics
Tietokannassa oleva lehden nimi: ASTRONOMY & ASTROPHYSICS
Lehden akronyymi: ASTRON ASTROPHYS
Artikkelin numero: ARTN A9
Vuosikerta: 642
Sivujen määrä: 11
ISSN: 0004-6361
eISSN: 1432-0746
DOI: https://doi.org/10.1051/0004-6361/201937257
Rinnakkaistallenteen osoite: https://research.utu.fi/converis/portal/detail/Publication/50709159
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.
Ladattava julkaisu This is an electronic reprint of the original article. |  |
