火星着陆发动机羽流与火壤的相互作用

doi:10.7527/S1000-6893.2021.26557

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2022, Vol. 43 ›› Issue (3): 626557-626557.doi: 10.7527/S1000-6893.2021.26557

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

Abstract

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

CLC Number:

V417

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.

References

[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).

Interaction between engine plume and Martian soil during Mars landing

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