Experimental Study on Thermal Vacuum Environment Sensitivity of Spacecraft Antenna's Typical Failure

With the development of space applications, spacecraft antenna has become an indispensable part of any space system. The spacecraft antenna affects and constrains the performance and functionality of the entire wireless communication system as well as the entire spacecraft. Spacecraft antenna has to...

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Main Authors: Bi Yanqiang, Wang Jing, Qie Dianfu, Yonghong Shang, Li Xiyuan
Format: Article
Language:English
Published: EDP Sciences 2017-01-01
Series:MATEC Web of Conferences
Online Access:https://doi.org/10.1051/matecconf/201711403012
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author Bi Yanqiang
Wang Jing
Qie Dianfu
Yonghong Shang
Li Xiyuan
author_facet Bi Yanqiang
Wang Jing
Qie Dianfu
Yonghong Shang
Li Xiyuan
author_sort Bi Yanqiang
collection DOAJ
description With the development of space applications, spacecraft antenna has become an indispensable part of any space system. The spacecraft antenna affects and constrains the performance and functionality of the entire wireless communication system as well as the entire spacecraft. Spacecraft antenna has to withstand the noise, vibration, shock and acceleration as launched, and weightlessness, high vacuum, radiation, extreme hot and cold alternating space environment on-orbit[1].The influence of different environmental factors on the typical failure modes of spacecraft antenna is different. The environmental adaptability of the spacecraft antenna depends mainly on its structural design, material, process and other factors. In this paper, the influence of different environmental factors on the typical failure modes of the spacecraft antenna is studied. The sensitivity analysis of the typical failure modes of the thermal vacuum environment is verified by experiments, which provides support for the development of the spacecraft antenna.
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spelling doaj.art-0deee58f265e43e6bbd0b30d8e5677ba2022-12-21T23:28:09ZengEDP SciencesMATEC Web of Conferences2261-236X2017-01-011140301210.1051/matecconf/201711403012matecconf_2mae2017_03012Experimental Study on Thermal Vacuum Environment Sensitivity of Spacecraft Antenna's Typical FailureBi YanqiangWang JingQie DianfuYonghong ShangLi XiyuanWith the development of space applications, spacecraft antenna has become an indispensable part of any space system. The spacecraft antenna affects and constrains the performance and functionality of the entire wireless communication system as well as the entire spacecraft. Spacecraft antenna has to withstand the noise, vibration, shock and acceleration as launched, and weightlessness, high vacuum, radiation, extreme hot and cold alternating space environment on-orbit[1].The influence of different environmental factors on the typical failure modes of spacecraft antenna is different. The environmental adaptability of the spacecraft antenna depends mainly on its structural design, material, process and other factors. In this paper, the influence of different environmental factors on the typical failure modes of the spacecraft antenna is studied. The sensitivity analysis of the typical failure modes of the thermal vacuum environment is verified by experiments, which provides support for the development of the spacecraft antenna.https://doi.org/10.1051/matecconf/201711403012
spellingShingle Bi Yanqiang
Wang Jing
Qie Dianfu
Yonghong Shang
Li Xiyuan
Experimental Study on Thermal Vacuum Environment Sensitivity of Spacecraft Antenna's Typical Failure
MATEC Web of Conferences
title Experimental Study on Thermal Vacuum Environment Sensitivity of Spacecraft Antenna's Typical Failure
title_full Experimental Study on Thermal Vacuum Environment Sensitivity of Spacecraft Antenna's Typical Failure
title_fullStr Experimental Study on Thermal Vacuum Environment Sensitivity of Spacecraft Antenna's Typical Failure
title_full_unstemmed Experimental Study on Thermal Vacuum Environment Sensitivity of Spacecraft Antenna's Typical Failure
title_short Experimental Study on Thermal Vacuum Environment Sensitivity of Spacecraft Antenna's Typical Failure
title_sort experimental study on thermal vacuum environment sensitivity of spacecraft antenna s typical failure
url https://doi.org/10.1051/matecconf/201711403012
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AT wangjing experimentalstudyonthermalvacuumenvironmentsensitivityofspacecraftantennastypicalfailure
AT qiedianfu experimentalstudyonthermalvacuumenvironmentsensitivityofspacecraftantennastypicalfailure
AT yonghongshang experimentalstudyonthermalvacuumenvironmentsensitivityofspacecraftantennastypicalfailure
AT lixiyuan experimentalstudyonthermalvacuumenvironmentsensitivityofspacecraftantennastypicalfailure