航空学报 > 2022, Vol. 43 Issue (3): 626557-626557   doi: 10.7527/S1000-6893.2021.26557

火星着陆发动机羽流与火壤的相互作用

叶青1, 饶炜1, 刘锋2, 孙泽洲1, 刘国强1, 王闯1, 董捷1, 韩泉东2, 缪远明1, 谭志云1, 陆慧林3   

  1. 1. 北京空间飞行器总体设计部, 北京 100094;
    2. 上海空间推进研究所, 上海 201112;
    3. 哈尔滨工业大学 能源科学与工程学院, 哈尔滨 150006
  • 收稿日期:2021-10-25 修回日期:2021-11-15 出版日期:2022-03-15 发布日期:2021-12-24
  • 通讯作者: 叶青 E-mail:yefeng7554@163.com
  • 基金资助:
    国家重大科技专项

Interaction between engine plume and Martian soil during Mars landing

YE Qing1, RAO Wei1, LIU Feng2, SUN Zezhou1, LIU Guoqiang1, WANG Chuang1, DONG Jie1, HAN Quandong2, MIAO Yuanming1, TAN Zhiyun1, LU Huilin3   

  1. 1. Beijing Institute of Spacecraft System Engineering, Beijing 100094, China;
    2. Shanghai Institute of Space Propulsion, Shanghai 201112, China;
    3. School of Energy Science and Engineering, Harbin Institute of Technology, Harbin 150006, China
  • Received:2021-10-25 Revised:2021-11-15 Online:2022-03-15 Published:2021-12-24
  • Supported by:
    National Science and Technology Major Project

摘要: 火星探测器着陆过程中的发动机羽流与火壤发生复杂的相互作用,一方面探测器底部的火壤表面成分及分布形式被破坏,影响探测器的着陆过程;另一方面受发动机羽流作用而扬起和悬浮的颗粒,会影响探测装置的可靠工作。针对此问题,利用数值模拟,对火星探测器着陆过程中的发动机羽流和火壤相互作用进行了研究,获得了不同发动机高度和推力下火壤颗粒的激扬高度、火坑深度和火坑宽度,通过在轨飞行数据反演对仿真算法进行了验证和评价,为火星着陆策略的制定提供了支撑。

关键词: 火星着陆, 羽流, 火壤, 两相流分析, 飞行数据

Abstract: During the landing process of Mars Rover, there is complex interaction between the engine plume and Martian soil, which on the one hand, affects the landing process due to the destruction of the composition and distribution form of Martian soil surface at the bottom of the Rover; and on the other, affects the reliable operation of detection device due to the particles raised and suspended under the action of the engine plume.In this connection, the paper studies the interaction between engine plume and Martian soil during the landing process of Mars Rover through numerical simulation, obtains the raising height of Martian soil particles as well as pit depth and width under different engine heights and thrusts, and verifies and evaluates the simulation algorithm via the in-orbit flight data inversion, so as to provide a support for the formulation of Mars landing strategy.

Key words: Mars landing, plume, Martian soil, two-phase flow analysis, flight data

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