空间项目“ionosat - micro”:准备实施

Pub Date : 2022-12-08 DOI:10.15407/knit2022.06.003
G. Lizunov, V. Korepanov, A. Lukenyuk, O. Piankova, O. P. Fedorov
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引用次数: 0

摘要

Ionosat-Micro是一个致力于近地空间研究的基础科学项目。该项目被认为是对现代空间天气知识发展和电离层对地表能源(如天气现象、电力线运行、地震及其准备过程、强大的技术危害等)的响应所带来的挑战的回答。此外,Ionosat-Micro项目是先前电离层任务的逻辑延续和补充,例如Dynamics Explorer 2(1982年发射)、Freja(1992年)、DEMETER(2004年)、Swarm(2013年)和CSES(2018年)。该项目是在乌克兰国家空间方案和乌克兰国家科学院科学空间研究方案的支持和框架内编制的。文章概述了该项目的科学原理,描述了正在创建的空间系统的参数,以及科学设备的组成和运行逻辑。该项目将在卫星平台Microsat-M上实施,该平台由中国国家设计局设计,用于进行科学和技术实验。计划发射的卫星轨道为圆形太阳同步轨道,倾角98度,高度600-700公里(轨道参数、发射方式和发射日期正在确定中)。Ionosat-Micro有效载荷包括一套科学仪器,用于记录中性大气和等离子体的整体结构和物理参数,空间电流系统和地磁场的结构和参数,以及超低频-超低频-超低频电磁扰动的频谱和波形。测量数据收集、处理和分发中心是为了积累和有针对性的数据处理而创建的。
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SPACE PROJECT “IONOSAT – MICRO”: READINESS FOR IMPLEMENTATION
Ionosat-Micro is a fundamental scientific project devoted to the study of near-Earth space. The project is conceived as an answer to the challenges posed by the modern development of knowledge about Space Weather and the ionospheric responses to surface energy sources (such as weather phenomena, power lines operation, earthquakes and processes of their preparation, powerful technogenic hazards, etc.). Furthermore, the project Ionosat-Micro is a logical continuation and addition to previous ionospheric missions, such as Dynamics Explorer 2 (launched in 1982), Freja (1992), DEMETER (2004), Swarm (2013), and CSES (2018). The project is being prepared with the support and within the framework of The National Space Program of Ukraine and The Program of the National Academy of Sciences of Ukraine for Scientific Space Research. The article outlines the scientific principles of the project, describes the parameters of the space system being created, and the composition and operation logic of the scientific equipment. The project is to be implemented on board the satellite platform Microsat-M, which has been designed by Yuzhnoye State Design Office to conduct scientific and technological experiments. The planned satellite orbit is circular sun-synchronous with an inclination of 98 degrees and altitude of 600–700 km (orbital parameters, method and date of the launch are being clarified). Ionosat-Micro payload includes a set of scientific instruments designed to register the global structure and physical parameters of the neutral atmosphere and plasma, the structure and parameters of the space current systems and geomagnetic field, as well as the spectra and wave-forms of ULF-ELF-VLF electromagnetic perturbations. The Center for Collection, Processing, and Distribution of Measurement Data was created for the purpose of accumulating and targeted data processing.
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