Modeling and Simulation of Supersonic Parachute Inflation in Mars Environment

被引：0

作者：

Zhao, Miao ^{[1
,2
]}

Zhang, Sijun ^{[3
]}

Zhang, Zhang ^{[1
,2
]}

Wang, Qi ^{[1
,2
]}

Liu, Yu ^{[1
,2
]}

Li, Jian ^{[1
,2
]}

机构：

[1] Beijing Inst Space Mech & Elect, Beijing 100094, Peoples R China

[2] CASC, Lab Aerosp Entry Descent & Landing Technol, Beijing 100094, Peoples R China

[3] ESI US R&D Inc, 620 Discovery Dr,STE 120,Bldg 2, Huntsville, AL 35806 USA

来源：

MAN-MACHINE-ENVIRONMENT SYSTEM ENGINEERING, MMESE | 2022年 / 800卷

关键词：

Disk-gap-band parachute; Supersonic; ALE method; Mars probe landing; Fluid-Structure Interaction (FSI);

D O I：

10.1007/978-981-16-5963-8_62

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

Parachute plays an important role of aerodynamic deceleration during exploration and landing. In this paper, inflation process of a disk-gap-band parachute in low-density and supersonic airflow is simulated based on the Arbitrary Lagrange Euler (ALE) method. Firstly, the fluid-structure interaction (FSI) numerical model of the parachute has been built. Then, the inflation process is simulated in Mars environment at Ma = 2. The simulation result shows the inflation time is 0.135 s, and after parachute reaches the over inflation stage, the canopy and the suspension line oscillate slightly, which can provide an important reference for the design of Mars parachute.

引用

页码：445 / 451

页数：7

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