Development of 6 U CubeSat’s Deployable Solar Panel with Burn Wire Triggering Holding and Release Mechanism
Joint Authors
Oh, Hyun-Ung
Park, Tae-Yong
Chae, Bong-Geon
Source
International Journal of Aerospace Engineering
Issue
Vol. 2019, Issue 2019 (31 Dec. 2019), pp.1-13, 13 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2019-04-30
Country of Publication
Egypt
No. of Pages
13
Abstract EN
In the present work, a deployable solar panel based on a burn wire triggering holding and release mechanism was developed for use of 6 U CubeSat.
The holding and release mechanism was designed based on a nichrome burn wire cutting method widely used for CubeSat applications.
However, it provides a high loading capability, reliable wire cutting, multiplane constraints, and handling simplicity during the tightening process of wire.
A demonstration model of a printed circuit board-based solar panel stiffened by a high-pressure fiberglass-laminated G10 material was fabricated and tested to validate the effectiveness of the design and functionality of the mechanism under various test conditions.
The structural safety of the solar panel combined with the mechanism in a launch vibration environment was verified through sine and random vibration tests at qualification level.
American Psychological Association (APA)
Park, Tae-Yong& Chae, Bong-Geon& Oh, Hyun-Ung. 2019. Development of 6 U CubeSat’s Deployable Solar Panel with Burn Wire Triggering Holding and Release Mechanism. International Journal of Aerospace Engineering،Vol. 2019, no. 2019, pp.1-13.
https://search.emarefa.net/detail/BIM-1156901
Modern Language Association (MLA)
Park, Tae-Yong…[et al.]. Development of 6 U CubeSat’s Deployable Solar Panel with Burn Wire Triggering Holding and Release Mechanism. International Journal of Aerospace Engineering No. 2019 (2019), pp.1-13.
https://search.emarefa.net/detail/BIM-1156901
American Medical Association (AMA)
Park, Tae-Yong& Chae, Bong-Geon& Oh, Hyun-Ung. Development of 6 U CubeSat’s Deployable Solar Panel with Burn Wire Triggering Holding and Release Mechanism. International Journal of Aerospace Engineering. 2019. Vol. 2019, no. 2019, pp.1-13.
https://search.emarefa.net/detail/BIM-1156901
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1156901
