The CUSP CubeSat mission for space weather multi-physics analysis, design, and testing
CUSP CubeSat 任务的空间天气多物理分析、设计与测试
The CUbesat Solar Polarimeter (CUSP) mission aims to measure the linear polarization of solar flares in the hard X-ray band by means of a Compton scattering polarimeter. CUSP is a project in the framework of the Alcor Program of the Italian Space Agency aimed at developing new CubeSat missions. We present the outcomes of the CUSP's Phase B study, which is ended on 2 July 2026. The design solutions adopted for the mission's most critical multi-physics design drivers will be discussed, these solutions have been formulated and applied to demonstrate compliance with system requirements at both the spacecraft and platform levels. Moreover, we will discuss the validation of the Payload model based on the environmental testing campaign (e.g., vibration) carried out on a demonstrator.
展开 ▾将飞行代表性结构模型用于有限元模型与鉴定级三轴振动测试的相关性验证,首阶模态约 595 Hz、试验前后无结构退化;为 6U XL CubeSat 太阳硬 X 射线偏振载荷确立可追溯的结构验证基线。
该任务延续了意大利航天局 Alcor 计划下基于 CubeSat 星座开展太阳耀斑硬 X 射线偏振测量的路线,任务概述已在 Fabiani+ 2022 和 Fabiani+ 2024 中给出;多物理场分析与载荷设计则由 Lombardi+ 2024 和 Lombardi+ 2025 推进。本文在 Phase B 阶段聚焦前端单元的结构验证,将飞行代表性结构模型与有限元模态/随机振动分析联合,并完成鉴定级三轴振动试验与模型相关性工作。结果表明首阶模态约 595 Hz、试验前后无结构退化,确立了后续 EQM 与飞行准备阶段的结构基线。展望未来,此类小型化平台的高刚度轻量化设计方法有望加速空间天气任务载荷迭代,并推广到多载荷 CubeSat 复杂动力学验证。
预印本 2026-07-31 · 收录 2026-08-20