Study on Numerical Simulation Methods for Hypervelocity Impact on Large-Scale Complex Spacecraft Structures

Study on Numerical Simulation Methods for Hypervelocity Impact on Large-Scale Complex Spacecraft Structures

This paper aims to study the difference of results in breakup state judgment, debris cloud and fragment characteristic parameter during hypervelocity impact (HVI) on large-scale complex spacecraft structures by various numerical simulation methods. We compared the results of the test of aluminum pro...

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Bibliographic Details
Main Authors: Yanxi Zhang, Fengjiang An, Shasha Liao, Cheng Wu, Jian Liu, Yipeng Li
Format: Article
Language:English
Published: MDPI AG 2021-12-01
Series:Aerospace
Subjects:
hypervelocity impact
numerical simulation
finite element method-smooth particle hydrodynamics adaptive coupling method
smooth particle hydrodynamics method
satellite damage
Online Access:https://www.mdpi.com/2226-4310/9/1/12

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