Origami-based Deployable Reflector Structure Using Flasher Pattern플래셔 패턴을 활용한 종이접기 기반의 전개형 반사판 구조물

Cited 0 time in webofscience Cited 0 time in scopus
  • Hit : 107
  • Download : 0
The development of small satellite payloads in current times requires efficient use of limited space, while achieving high performance. For high-performance missions, reflector antennas with a certain size or larger may be necessary, but spatial constraints can pose a challenge. To overcome these limitations, researchers are designing these structures in deployable configurations.In this research, we propose the origami-based deployable structure, which can be easily and efficiently packed. The structure is able to deploy itself by applying a compliant flexure hinge. In order to evaluate the performance of the proposed deployable reflector structure, the packaging efficiency, surface error, and focus error are analyzed in relation to changing the design parameter. A deployable prototype is constructed using a torsion-based compliant hinge. Finally, the position change of specific points is experimentally measured to analyze a deployment repeatability.
Publisher
KOREAN SOC AERONAUTICAL & SPACE SCIENCES
Issue Date
2023
Language
English
Article Type
Article
Citation

JOURNAL OF THE KOREAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, v.51, no.7, pp.443 - 452

ISSN
1225-1348
DOI
10.5139/JKSAS.2023.51.7.443
URI
http://hdl.handle.net/10203/311751
Appears in Collection
AE-Journal Papers(저널논문)
Files in This Item
There are no files associated with this item.

qr_code

  • mendeley

    citeulike


rss_1.0 rss_2.0 atom_1.0