Lugaz Noé, Lee Christina O, Al-Haddad Nada, Lillis Robert J, Jian Lan K, Curtis David W, Galvin Antoinette B, Whittlesey Phyllis L, Rahmati Ali, Zesta Eftyhia, Moldwin Mark, Summerlin Errol J, Larson Davin E, Courtade Sasha, French Richard, Hunter Richard, Covitti Federico, Cosgrove Daniel, Prall J D, Allen Robert C, Zhuang Bin, Winslow Réka M, Scolini Camilla, Lynch Benjamin J, Filwett Rachael J, Palmerio Erika, Farrugia Charles J, Smith Charles W, Möstl Christian, Weiler Eva, Janvier Miho, Regnault Florian, Livi Roberto, Nieves-Chinchilla Teresa
Institute for the Study of Earth, Oceans, and Space, University of New Hampshire, Durham, NH 03824 USA.
Space Sciences Laboratory, University of California, Berkeley, CA 94720 USA.
Space Sci Rev. 2024;220(7):73. doi: 10.1007/s11214-024-01108-8. Epub 2024 Sep 20.
Based on decades of single-spacecraft measurements near 1 au as well as data from heliospheric and planetary missions, multi-spacecraft simultaneous measurements in the inner heliosphere on separations of 0.05-0.2 au are required to close existing gaps in our knowledge of solar wind structures, transients, and energetic particles, especially coronal mass ejections (CMEs), stream interaction regions (SIRs), high speed solar wind streams (HSS), and energetic storm particle (ESP) events. The Mission to Investigate Interplanetary Structures and Transients (MIIST) is a concept for a small multi-spacecraft mission to explore the near-Earth heliosphere on these critical scales. It is designed to advance two goals: (a) to determine the spatiotemporal variations and the variability of solar wind structures, transients, and energetic particle fluxes in near-Earth interplanetary (IP) space, and (b) to advance our fundamental knowledge necessary to improve space weather forecasting from data. We present the scientific rationale for this proposed mission, the science requirements, payload, implementation, and concept of mission operation that address a key gap in our knowledge of IP structures and transients within the cost, launch, and schedule limitations of the NASA Heliophysics Small Explorers program.
基于数十年来在1天文单位附近进行的单航天器测量以及来自日球层和行星任务的数据,需要在日球层内部以0.05 - 0.2天文单位的间距进行多航天器同步测量,以填补我们在太阳风结构、瞬变和高能粒子(特别是日冕物质抛射(CME)、流相互作用区域(SIR)、高速太阳风流(HSS)和高能风暴粒子(ESP)事件)知识方面的现有空白。行星际结构和瞬变探测任务(MIIST)是一个小型多航天器任务的概念,旨在在这些关键尺度上探索近地日球层。它旨在推进两个目标:(a)确定近地行星际(IP)空间中太阳风结构、瞬变和高能粒子通量的时空变化及变异性,以及(b)从数据推进我们改善空间天气预报所需的基础知识。我们阐述了这一拟议任务的科学依据、科学要求、有效载荷、实施情况以及任务操作概念,这些内容在NASA日球物理学小型探索者计划的成本、发射和进度限制范围内,解决了我们在IP结构和瞬变知识方面的一个关键空白。