火星着陆发动机羽流与火壤的相互作用

doi:10.7527/S1000-6893.2021.26557

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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. 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. 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/Abstract

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

中图分类号:

V417

叶青, 饶炜, 刘锋, 孙泽洲, 刘国强, 王闯, 董捷, 韩泉东, 缪远明, 谭志云, 陆慧林. 火星着陆发动机羽流与火壤的相互作用[J]. 航空学报, 2022, 43(3): 626557-626557.

YE Qing, RAO Wei, LIU Feng, SUN Zezhou, LIU Guoqiang, WANG Chuang, DONG Jie, HAN Quandong, MIAO Yuanming, TAN Zhiyun, LU Huilin. Interaction between engine plume and Martian soil during Mars landing[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(3): 626557-626557.

参考文献

[1] HUTTON R E, MOORE H J, SCOTT R F, et al.Surface erosion caused on Mars from Viking descent engine plume[J].The Moon and the Planets, 1980, 23(3):293-305.
[2] SCOTT R.Apollo program soil mechanics experiment:NASA-CR-144438[R].Washinton, D.C.:NASA, 1975.
[3] IMMER C, METZGER P, HINTZE P E, et al.Apollo 12 Lunar Module exhaust plume impingement on Lunar Surveyor III[J].Icarus, 2011, 211(2):1089-1102.
[4] LIEVER P, TOSH A, ARSLANBEKOV R, et al.Modeling of rocket plume impingement flow and debris transport in lunar environment[C]//50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition.Reston:AIAA, 2012.
[5] KUANG S B, LAMARCHE C Q, CURTIS J S, et al.Discrete particle simulation of jet-induced cratering of a granular bed[J].Powder Technology, 2013, 239:319-336.
[6] 王淑彦.二维拱形模拟体作用下月尘颗粒悬浮过程研究[C]//2007多相流学术会议, 2007. WANG S Y.Study on the suspension process of dust particles by two-dimensional arch simulation[C]//2007 Conference on Multiphase Flow, 2007(in Chinese).
[7] 陆鑫, 黄勇, 李雯, 等.着陆作用下月尘激扬的三维离散元分析[J].航天器工程, 2011, 20(1):101-108. LU X, HUANG Y, LI W, et al.3-D DEM analysis of lunar dust levitation characteristics during landing progress[J].Spacecraft Engineering, 2011, 20(1):101-108(in Chinese).
[8] 耿动梁, 任德鹏, 叶青, 等.羽流场与月壤颗粒相互作用的一种新计算方法[J].宇航学报, 2014, 35(8):884-892. GENG D L, REN D P, YE Q, et al.A new computational method for the interaction between plume field and soil particles[J].Journal of Astronautics, 2014, 35(8):884-892(in Chinese).
[9] 郑刚, 崔玉红, 于伟, 等.考虑相互碰撞影响的月壤颗粒运动轨迹计算方法研究[J].空间科学学报, 2015, 35(4):486-494. ZHENG G, CUI Y H, YU W, et al.Method on calculation of lunar soil particles trajectories considering collision effect[J].Chinese Journal of Space Science, 2015, 35(4):486-494(in Chinese).
[10] 邵亦琪, 崔玉红, 郑刚, 等.真空环境下月壤颗粒受力影响因素及对空间分布的影响[J].空间科学学报, 2016, 36(1):1-11. SHAO Y Q, CUI Y H, ZHENG G, et al.Study on force-influencing factors and spatial distribution of lunar regolith particles under vacuum environment[J].Chinese Journal of Space Science, 2016, 36(1):1-11(in Chinese).

E-mail：hkxb@buaa.edu.cn

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火星着陆发动机羽流与火壤的相互作用

Interaction between engine plume and Martian soil during Mars landing

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