Design and Analysis of Micro-Satellite Whip Antenna Rotating Disk Deployable Mechanism

Han Jin; Wang Xinsheng

doi:doi:10.11648/j.sd.20160406.18

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Design and Analysis of Micro-Satellite Whip Antenna Rotating Disk Deployable Mechanism

Han Jin, Wang Xinsheng

Published in Science Discovery (Volume 4, Issue 6)

Received: 29 November 2016 Accepted: Published: 1 December 2016

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Abstract

The structure of the micro-satellite is exquisite and compact which requires the long whip antenna to be tucked into the specific deployable mechanism. This paper analyses the advantages and disadvantages of commonly used the swing arm deployable mechanism and on this basis we design a kind of rotating disk deployable mechanism. By the mechanics analysis and comparison of this two mechanism, the superiority of the new mechanism on the mechanical and dynamic performance was proved. This design and the conclusion has great significance in futher research.

Published in	Science Discovery (Volume 4, Issue 6)
DOI	10.11648/j.sd.20160406.18
Page(s)	393-397
Creative Commons	This is an Open Access article, distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution and reproduction in any medium or format, provided the original work is properly cited.
Copyright	Copyright © The Author(s), 2024. Published by Science Publishing Group

Keywords

Whip Antenna, Deployable Mechanism, Rotating Disk, Mechanics Analysis

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APA Style

Han Jin, Wang Xinsheng. (2016). Design and Analysis of Micro-Satellite Whip Antenna Rotating Disk Deployable Mechanism. Science Discovery, 4(6), 393-397. https://doi.org/10.11648/j.sd.20160406.18

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ACS Style

Han Jin; Wang Xinsheng. Design and Analysis of Micro-Satellite Whip Antenna Rotating Disk Deployable Mechanism. Sci. Discov. 2016, 4(6), 393-397. doi: 10.11648/j.sd.20160406.18

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AMA Style

Han Jin, Wang Xinsheng. Design and Analysis of Micro-Satellite Whip Antenna Rotating Disk Deployable Mechanism. Sci Discov. 2016;4(6):393-397. doi: 10.11648/j.sd.20160406.18

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@article{10.11648/j.sd.20160406.18,
  author = {Han Jin and Wang Xinsheng},
  title = {Design and Analysis of Micro-Satellite Whip Antenna Rotating Disk Deployable Mechanism},
  journal = {Science Discovery},
  volume = {4},
  number = {6},
  pages = {393-397},
  doi = {10.11648/j.sd.20160406.18},
  url = {https://doi.org/10.11648/j.sd.20160406.18},
  eprint = {https://article.sciencepublishinggroup.com/pdf/10.11648.j.sd.20160406.18},
  abstract = {The structure of the micro-satellite is exquisite and compact which requires the long whip antenna to be tucked into the specific deployable mechanism. This paper analyses the advantages and disadvantages of commonly used the swing arm deployable mechanism and on this basis we design a kind of rotating disk deployable mechanism. By the mechanics analysis and comparison of this two mechanism, the superiority of the new mechanism on the mechanical and dynamic performance was proved. This design and the conclusion has great significance in futher research.},
 year = {2016}
}

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TY  - JOUR
T1  - Design and Analysis of Micro-Satellite Whip Antenna Rotating Disk Deployable Mechanism
AU  - Han Jin
AU  - Wang Xinsheng
Y1  - 2016/12/01
PY  - 2016
N1  - https://doi.org/10.11648/j.sd.20160406.18
DO  - 10.11648/j.sd.20160406.18
T2  - Science Discovery
JF  - Science Discovery
JO  - Science Discovery
SP  - 393
EP  - 397
PB  - Science Publishing Group
SN  - 2331-0650
UR  - https://doi.org/10.11648/j.sd.20160406.18
AB  - The structure of the micro-satellite is exquisite and compact which requires the long whip antenna to be tucked into the specific deployable mechanism. This paper analyses the advantages and disadvantages of commonly used the swing arm deployable mechanism and on this basis we design a kind of rotating disk deployable mechanism. By the mechanics analysis and comparison of this two mechanism, the superiority of the new mechanism on the mechanical and dynamic performance was proved. This design and the conclusion has great significance in futher research.
VL  - 4
IS  - 6
ER  -

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Author Information

Han Jin

School of Astronautics, Beihang University, Beijing, China
Wang Xinsheng

School of Astronautics, Beihang University, Beijing, China

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APA Style

Han Jin, Wang Xinsheng. (2016). Design and Analysis of Micro-Satellite Whip Antenna Rotating Disk Deployable Mechanism. Science Discovery, 4(6), 393-397. https://doi.org/10.11648/j.sd.20160406.18

Copy | Download

ACS Style

Han Jin; Wang Xinsheng. Design and Analysis of Micro-Satellite Whip Antenna Rotating Disk Deployable Mechanism. Sci. Discov. 2016, 4(6), 393-397. doi: 10.11648/j.sd.20160406.18

Copy | Download

AMA Style

Han Jin, Wang Xinsheng. Design and Analysis of Micro-Satellite Whip Antenna Rotating Disk Deployable Mechanism. Sci Discov. 2016;4(6):393-397. doi: 10.11648/j.sd.20160406.18

Copy | Download

@article{10.11648/j.sd.20160406.18,
  author = {Han Jin and Wang Xinsheng},
  title = {Design and Analysis of Micro-Satellite Whip Antenna Rotating Disk Deployable Mechanism},
  journal = {Science Discovery},
  volume = {4},
  number = {6},
  pages = {393-397},
  doi = {10.11648/j.sd.20160406.18},
  url = {https://doi.org/10.11648/j.sd.20160406.18},
  eprint = {https://article.sciencepublishinggroup.com/pdf/10.11648.j.sd.20160406.18},
  abstract = {The structure of the micro-satellite is exquisite and compact which requires the long whip antenna to be tucked into the specific deployable mechanism. This paper analyses the advantages and disadvantages of commonly used the swing arm deployable mechanism and on this basis we design a kind of rotating disk deployable mechanism. By the mechanics analysis and comparison of this two mechanism, the superiority of the new mechanism on the mechanical and dynamic performance was proved. This design and the conclusion has great significance in futher research.},
 year = {2016}
}

Copy | Download

TY  - JOUR
T1  - Design and Analysis of Micro-Satellite Whip Antenna Rotating Disk Deployable Mechanism
AU  - Han Jin
AU  - Wang Xinsheng
Y1  - 2016/12/01
PY  - 2016
N1  - https://doi.org/10.11648/j.sd.20160406.18
DO  - 10.11648/j.sd.20160406.18
T2  - Science Discovery
JF  - Science Discovery
JO  - Science Discovery
SP  - 393
EP  - 397
PB  - Science Publishing Group
SN  - 2331-0650
UR  - https://doi.org/10.11648/j.sd.20160406.18
AB  - The structure of the micro-satellite is exquisite and compact which requires the long whip antenna to be tucked into the specific deployable mechanism. This paper analyses the advantages and disadvantages of commonly used the swing arm deployable mechanism and on this basis we design a kind of rotating disk deployable mechanism. By the mechanics analysis and comparison of this two mechanism, the superiority of the new mechanism on the mechanical and dynamic performance was proved. This design and the conclusion has great significance in futher research.
VL  - 4
IS  - 6
ER  -

Copy | Download