항공우주시스템공학회지 (Journal of Aerospace System Engineering)

  • 제15권4호
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  • Pages.1-6
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  • 2021
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  • 1976-6300(pISSN)
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  • 2508-7150(eISSN)
항공우주시스템공학회 (The Society for Aerospace System Engineering)
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A Study on the Nylon Wire Holding and Release Mechanism for Cube Satellites by Applying Constant Holding

  • Koo, KeonWoo (Department of Aerospace and Software Engineering, Gyeongsang National University)
  • 투고 : 2021.01.13
  • 심사 : 2021.04.12
  • 발행 : 2021.08.31
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초록

The non-explosive holding and release mechanism is used to prevent damage to the mission component caused by explosives when the deployment structure for Cube Satellites is separated. However, among the several types available, the non-explosive holding and release mechanism system using nylon wires depend on the nylon wire knot method and tightening power of the worker. Therefore, in this study, we conducted experiments with the operation of a new holding and release mechanism system by conceptualizing the Boa System Dial, which can provide a constant tightening force regardless of worker proficiency and deploying a imitational solar panel. In this study, the process of binding and unbinding with constant tension was recorded while applying the novel non-explosive holding and release mechanism using the Boa System Dial proposed. In addition, required advances are indicated for the application of the proposed system to actual Cube Satellites.

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과제정보

This paper is a revised and supplemented version of the a paper presented at the 2020 Fall Conference of The Society for Aerospace System Engineering.

참고문헌

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