HYPERSONIC JET IMPINGEMENT DURING LANDING ON LUNAR AND MARTIAN SURFACES

登陆月球和火星表面期间的高超音速喷射撞击

• 批准号: 2887632
• 金额: --
• 依托单位: University of Glasgow
• 依托单位国家: 英国
• 项目类别: Studentship
• 财政年份: 2023
• 资助国家: 英国
• 起止时间: 2023 至 无数据
• 项目状态: 未结题
• 来源: https://gtr.ukri.org/projects?ref=studentship-2887632
• 关键词: HYPERSONIC; JET; IMPINGEMENT; DURING; LANDING

The proposed area of study is the complex and non-linear fluid dynamic interactions which occur between an ex- panding jet emitted from a spacecraft retro-propulsion rocket nozzle and the surface of a planetary body during a soft landing procedure, termed Plume Surface Interactions (PSI). The work will focus on the development and evaluation of a method of mitigating negative plume- surface effects by leveraging secondary flow to capture regolith ejecta, and simultaneously using supersonic fluidic injector technology to minimise plume-driven surface alteration. Unique to this proposal is the intended realisation of these goals using only spacecraft-borne hardware

提出的研究领域是软着陆过程中航天器反推火箭喷管喷出的膨胀喷流与行星体表面之间复杂的非线性流体动力学相互作用，称为羽流表面相互作用（PSI）。这项工作的重点是开发和评估一种方法，通过利用二次流捕获风化层喷出物来减轻羽流表面的负面影响，同时使用超音速射流喷射器技术来最大限度地减少羽流驱动的表面改变。该提案的独特之处在于，仅使用航天器携带的硬件就可以实现这些目标