Simulation Investigation of the Stowing and Deployment Processes of a Self-Deployable Sunshield

The stowing and deployment processes of a self-deployable sunshield are investigated numerically in this paper. The composition of the self-deployable sunshield is described. Deployed moment theoretical models for lenticular booms are formulated based on the bending theory of curved shell. The numer...

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Main Authors: Xu Cao, Yan Xu, Changhong Jiang, Qin Fang, Hao Feng
Format: Article
Language:English
Published: Hindawi Limited 2021-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2021/6672177
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spelling doaj-92ad1798af5047b182332a303d4b63b82021-02-22T00:02:10ZengHindawi LimitedInternational Journal of Aerospace Engineering1687-59742021-01-01202110.1155/2021/6672177Simulation Investigation of the Stowing and Deployment Processes of a Self-Deployable SunshieldXu Cao0Yan Xu1Changhong Jiang2Qin Fang3Hao Feng4Beijing Institute of Space Mechanics and ElectricitySchool of Aeronautics and AstronauticsBeijing Institute of Space Mechanics and ElectricitySchool of Aeronautics and AstronauticsBeijing Institute of Space Mechanics and ElectricityThe stowing and deployment processes of a self-deployable sunshield are investigated numerically in this paper. The composition of the self-deployable sunshield is described. Deployed moment theoretical models for lenticular booms are formulated based on the bending theory of curved shell. The numerical analysis method of deployed moment is proposed. Two types of control methods for a fold crease are presented, and a dynamic analysis model considering geometry and nonlinear contact is built. The analysis results indicate that the press flattening method can be used effectively for controlling the fold crease, and the analytical results of the deployed moment are very close to the theoretical results. A stowing and deployment process analysis of the self-deployable sunshield is conducted. Thus, the deployment configurations and the time history curves of the dynamic behaviors are obtained. The results verify the feasibility of the analysis model, and this study can provide technical support for the engineering application of the self-deployable sunshield.http://dx.doi.org/10.1155/2021/6672177
collection DOAJ
language English
format Article
sources DOAJ
author Xu Cao
Yan Xu
Changhong Jiang
Qin Fang
Hao Feng
spellingShingle Xu Cao
Yan Xu
Changhong Jiang
Qin Fang
Hao Feng
Simulation Investigation of the Stowing and Deployment Processes of a Self-Deployable Sunshield
International Journal of Aerospace Engineering
author_facet Xu Cao
Yan Xu
Changhong Jiang
Qin Fang
Hao Feng
author_sort Xu Cao
title Simulation Investigation of the Stowing and Deployment Processes of a Self-Deployable Sunshield
title_short Simulation Investigation of the Stowing and Deployment Processes of a Self-Deployable Sunshield
title_full Simulation Investigation of the Stowing and Deployment Processes of a Self-Deployable Sunshield
title_fullStr Simulation Investigation of the Stowing and Deployment Processes of a Self-Deployable Sunshield
title_full_unstemmed Simulation Investigation of the Stowing and Deployment Processes of a Self-Deployable Sunshield
title_sort simulation investigation of the stowing and deployment processes of a self-deployable sunshield
publisher Hindawi Limited
series International Journal of Aerospace Engineering
issn 1687-5974
publishDate 2021-01-01
description The stowing and deployment processes of a self-deployable sunshield are investigated numerically in this paper. The composition of the self-deployable sunshield is described. Deployed moment theoretical models for lenticular booms are formulated based on the bending theory of curved shell. The numerical analysis method of deployed moment is proposed. Two types of control methods for a fold crease are presented, and a dynamic analysis model considering geometry and nonlinear contact is built. The analysis results indicate that the press flattening method can be used effectively for controlling the fold crease, and the analytical results of the deployed moment are very close to the theoretical results. A stowing and deployment process analysis of the self-deployable sunshield is conducted. Thus, the deployment configurations and the time history curves of the dynamic behaviors are obtained. The results verify the feasibility of the analysis model, and this study can provide technical support for the engineering application of the self-deployable sunshield.
url http://dx.doi.org/10.1155/2021/6672177
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AT yanxu simulationinvestigationofthestowinganddeploymentprocessesofaselfdeployablesunshield
AT changhongjiang simulationinvestigationofthestowinganddeploymentprocessesofaselfdeployablesunshield
AT qinfang simulationinvestigationofthestowinganddeploymentprocessesofaselfdeployablesunshield
AT haofeng simulationinvestigationofthestowinganddeploymentprocessesofaselfdeployablesunshield
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