论文标题

太阳轨道任务 - 科学概述

The Solar Orbiter mission -- Science overview

论文作者

Müller, D., Cyr, O. C. St., Zouganelis, I., Gilbert, H. R., Marsden, R., Nieves-Chinchilla, T., Antonucci, E., Auchère, F., Berghmans, D., Horbury, T., Howard, R. A., Krucker, S., Maksimovic, M., Owen, C. J., Rochus, P., Rodriguez-Pacheco, J., Romoli, M., Solanki, S. K., Bruno, R., Carlsson, M., Fludra, A., Harra, L., Hassler, D. M., Livi, S., Louarn, P., Peter, H., Schühle, U., Teriaca, L., Iniesta, J. C. del Toro, Wimmer-Schweingruber, R. F., Marsch, E., Velli, M., De Groof, A., Walsh, A., Williams, D.

论文摘要

Solar Orbiter是ESA 2015 - 2025年宇宙愿景计划的第一个任务,以及ESA与NASA之间的国际合作任务,将从封闭式和外出探索太阳和Heliosphere。它于2020年2月10日启动,04:03 UTC来自Cape Canaveral,旨在解决与太阳如何创造和控制地球层有关的太阳能和地球物理学的关键问题,以及太阳活动为何随时间而变化。为了回答这些问题,该任务载有六种遥感仪器,以观察太阳和太阳电晕,以及四种原位仪器,以测量太阳风,能量颗粒和电磁场。在本文中,我们描述了任务的科学目标,以及船上工具的共同观察将如何解决这些目标。该论文首先总结了任务级的科学目标,然后概述了航天器和有效载荷。我们报告了每种仪器的可观察力和性能数字以及轨迹设计。接下来是科学操作概念的摘要。本文以对科学目标的更详细的描述结束。太阳轨道将在Heliosphere中的原位测量与太阳的高分辨率遥感观测结果结合在一起,以解决太阳能和地球物理学的基本问题。太阳能轨道有效载荷的性能满足了任务科学目标的要求。通过与其他太空任务和地面观测站的协调观察,将进一步增强其科学回报。

Solar Orbiter, the first mission of ESA's Cosmic Vision 2015-2025 programme and a mission of international collaboration between ESA and NASA, will explore the Sun and heliosphere from close up and out of the ecliptic plane. It was launched on 10 February 2020 04:03 UTC from Cape Canaveral and aims to address key questions of solar and heliospheric physics pertaining to how the Sun creates and controls the Heliosphere, and why solar activity changes with time. To answer these, the mission carries six remote-sensing instruments to observe the Sun and the solar corona, and four in-situ instruments to measure the solar wind, energetic particles, and electromagnetic fields. In this paper, we describe the science objectives of the mission, and how these will be addressed by the joint observations of the instruments onboard. The paper first summarises the mission-level science objectives, followed by an overview of the spacecraft and payload. We report the observables and performance figures of each instrument, as well as the trajectory design. This is followed by a summary of the science operations concept. The paper concludes with a more detailed description of the science objectives. Solar Orbiter will combine in-situ measurements in the heliosphere with high-resolution remote-sensing observations of the Sun to address fundamental questions of solar and heliospheric physics. The performance of the Solar Orbiter payload meets the requirements derived from the mission's science objectives. Its science return will be augmented further by coordinated observations with other space missions and ground-based observatories.

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