Horbury, T. S.O’Brien, H.Blazquez, I. CarrascoBendyk, M.Goldstein, Melvynet al2022-08-242022-08-242020-09-30“The Solar Orbiter magnetometer”, T.S. Horbury, H. O’Brien, I. Carrasco Blazquez, M. Bendyk, P. Brown, R. Hudson, V. Evans, T.M. Oddy, C.M. Carr, T.J. Beek, S. Bhattacharya, J.-A. Dominguez, L. Matthews, V.R. Myklebust, B. Whiteside, S. Bale, W. Baumjohann, B. Bavassano, D. Burgess, V. Carbone, P. Cargill, J. Eastwood, G. Erdös, L. Fletcher, R. Forsyth, J. Giacalone, K.-H. Glassmeier, M.L. Goldstein, T. Hoeksema, M. Lockwood, W. Magnes, M. Maksimovic, E. Marsch, W. Matthaeus, N. Murphy, V.M. Nakariakov, C.J. Owen, M. Owens, J. Rodriguez.-Pacheco, J.-L. Pincon, I. Richter, P. Riley, C. T. Russell, S. Schwartz, R. Vainio, M. Velli, S. Vennerstrom, R. Walsh, R.F. Wimmer-Schweingruber, G. Zank, D. Müller, Y. Zouganelis, A. Walsh, Astronomy and Astrophysics, 642, A9, https://doi.org/10.1051/0004-6361/201937257https://doi.org/10.1051/0004-6361/201937257http://hdl.handle.net/11603/25559Authors: T. S. Horbury, H. O’Brien, I. Carrasco Blazquez, M. Bendyk, P. Brown, R. Hudson, V. Evans, T. M. Oddy, C. M. Carr, T. J. Beek,†, E. Cupido, S. Bhattacharya, J.-A. Dominguez, L. Matthews, V. R. Myklebust, B. Whiteside, S. D. Bale, W. Baumjohann, D. Burgess, V. Carbone, P. Cargill, J. Eastwood, G. Erdös, L. Fletcher, R. Forsyth, J. Giacalone, K.-H. Glassmeier, M. L. Goldstein, T. Hoeksema, M. Lockwood, W. Magnes, M. Maksimovic, E. Marsch, W. H. Matthaeus, N. Murphy, V. M. Nakariakov, C. J. Owen, M. Owens, J. Rodriguez-Pacheco, I. Richter, P. Riley, C. T. Russell, S. Schwartz, R. Vainio, M. Velli, S. Vennerstrom, R. Walsh, R. F. Wimmer-Schweingruber, G. Zank, D. Müller, I. Zouganelis and A. P. WalshThe 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.11 pagesen-USThis work was written as part of one of the author's official duties as an Employee of the United States Government and is therefore a work of the United States Government. In accordance with 17 U.S.C. 105, no copyright protection is available for such works under U.S. Law.Public Domain Mark 1.0Text