通过标准偏差和发射度表征电力推进的羽散特性。

Journal of electric propulsion Pub Date : 2025-01-01 Epub Date: 2025-02-25 DOI:10.1007/s44205-025-00113-5
McKenna J D Breddan, Richard E Wirz
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引用次数: 0

摘要

电力推进系统需要仔细考虑在一系列操作条件和环境下的羽流发散和进化。现有的描述羽流散度的方法,如轮廓、羽流剖面和羽流快照,主要是由离群粒子控制的,不能提供可靠的或定量的见解。本文提出了用标准差和发射度来描述羽流发散的两种新方法,以定量地了解羽流物种的集体行为。此外,粒子加速器群落的发射度度量可以准确地描述羽流在二维位置和动量角空间中的演化。横截面发射度测量用于显示羽流演化中非哈密顿力的存在,即邻近粒子之间的随机库仑碰撞。最后,演示了全羽流发射度图作为一种识别电力推进羽流何时达到稳定状态的手段。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Plume divergence characterization for electric propulsion via standard deviation and emittance.

Electric propulsion systems require careful consideration of plume divergence and evolution over a range of operating conditions and environments. Existing means of describing plume divergence such as outlines, plume profiles, and snapshots of the plume are dominated by outlier particles and do not provide reliable or quantitative insight. Proposed herein are two novel methods for describing plume divergence using standard deviation and emittance to provide quantitative insight of the collective behavior of plume species. Furthermore, the emittance metric from the particle accelerator community is shown to accurately describe plume evolution in a two-dimensional position and momentum angle space. Cross-sectional emittance measurements are used to display the presence of non-Hamiltonian forces in plume evolution, namely stochastic Coulomb collisions between neighboring particles. Finally, full-plume emittance diagrams are demonstrated as a means of identifying when an electric propulsion plume has reached steady state.

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