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Ion temperature anisotropy across a magnetotail reconnection jet

A significant fraction of the energy released by magnetotail reconnection appears to go into ion heating, but this heating is generally anisotropic. We examine ARTEMIS dual‐spacecraft observations of a long‐duration magnetotail exhaust generated by antiparallel reconnection in conjunction with parti...

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Detalles Bibliográficos
Autores principales: Hietala, H., Drake, J. F., Phan, T. D., Eastwood, J. P., McFadden, J. P.
Formato: Online Artículo Texto
Lenguaje:English
Publicado: John Wiley and Sons Inc. 2015
Materias:
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC4950132/
https://www.ncbi.nlm.nih.gov/pubmed/27478283
http://dx.doi.org/10.1002/2015GL065168
Descripción
Sumario:A significant fraction of the energy released by magnetotail reconnection appears to go into ion heating, but this heating is generally anisotropic. We examine ARTEMIS dual‐spacecraft observations of a long‐duration magnetotail exhaust generated by antiparallel reconnection in conjunction with particle‐in‐cell simulations, showing spatial variations in the anisotropy across the outflow far (>100d (i)) downstream of the X line. A consistent pattern is found in both the spacecraft data and the simulations: While the total temperature across the exhaust is rather constant, near the boundaries T (i,||) dominates. The plasma is well above the firehose threshold within patchy spatial regions at |B (X)|∈[0.1,0.5]B (0), suggesting that the drive for the instability is strong and the instability is too weak to relax the anisotropy. At the midplane ( [Formula: see text]), T (i,⊥)>T (i,||) and ions undergo Speiser‐like motion despite the large distance from the X line.