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CEMP星HE 1005-1439中子俘获元素天体物理来源的研究
引用本文:汤靖师,屈颖莹,王琦.CEMP星HE 1005-1439中子俘获元素天体物理来源的研究[J].天文学报,2023(5):52-51.
作者姓名:汤靖师  屈颖莹  王琦
作者单位:南京大学天文与空间科学学院 南京 210023;现代天文与天体物理教育部重点实验室 南京 210023;南京大学空间环境与航天动力学研究所 南京 210023;北京跟踪与通信技术研究所 北京 100094
基金项目:国家自然科学基金项目(11873031)资助
摘    要:HE1005-1439是一颗金属丰度极低(Fe/H]~-3.0)的碳增丰贫金属星(Carbon Enhanced Metal-Poor,CEMP),该星的s-过程元素显著超丰(Ba/Fe]=1.16±0.31,Pb/Fe]=1.98±0.19),而r-过程元素温和超丰(Eu/Fe]=0.46±0.22),使用单一的s-过程模型和i-过程模型均不能拟合该星中子俘获丰度分布.采用丰度分解的方法探究该星化学元素的天体物理来源可有助于理解CEMP星的形成和化学演化.利用s-过程和r-过程的混合模型对其中子俘获元素的丰度分布进行拟合,发现该星的中子俘获元素主要来源于低质量低金属丰度AGB伴星的s-过程核合成,而r-过程核合成也有贡献.

关 键 词:恒星:丰度  恒星:形成  恒星:化学组成特殊
收稿时间:2022/7/20 0:00:00

Analysis and Design of Starlink-like Satellite Constellation
TANG Jing-shi,QU Ying-ying,WANG Qi.Analysis and Design of Starlink-like Satellite Constellation[J].Acta Astronomica Sinica,2023(5):52-51.
Authors:TANG Jing-shi  QU Ying-ying  WANG Qi
Institution:School of Astronomy and Space Science, Nanjing University, Nanjing 210023;Key Laboratory of Astronomy and Astrophysics, Ministry of Education, Nanjing 210023;Institute of Space Environment and Astrodynamics, Nanjing University, Nanjing 210023; Beijing Institute of Tracking and Telecommunication Technology, Beijing 100094
Abstract:Satellite constellations are widely used for communication, navigation and Earth observation purposes. They provide good ground coverages and serve better for these needs. Of all the configurations, the Walker constellation is extensively applied in many navigation satellite systems and some low Earth orbit communication constellations, since it can be easily designed and has good coverage. Despite of these advantages, the satellites in Walker constellation generally have different ground tracks. When multiple Walker constellations are to be coordinated, in terms that the orbital planes precess synchronously with the same satellite mean motion $\Omega_1$, the semi-major axes of these Walker constellations would be significantly different even when the orbital inclinations differ by a small amount. The Space Exploration Corp (SpaceX) claimed a new constellation design in a patent for their multi-shell Starlink satellite constellation. Constellation shells with different inclinations have small altitude differences, which facilitates regulatory approval and deployment. Satellites in the same shell can also be easily designed to share the same ground track. Although they claimed these features in the patent, SpaceX shared little technical details regarding how to design these constellations. Here in this paper, we analyze the features of the Starlink constellation and try to find a practical approach to design a Starlink-like constellation, as well as how to determine the rules for inter-satellite links within the constellation.
Keywords:celestial mechanics: satellite orbit  celestial mechanics: constellation design  space vehicle: Starlink
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