High Damping Passive Launch Vibration Isolation System Using Superelastic SMA with Multilayered Viscous Lamina

Whole-spacecraft launch-vibration isolation systems are attractive for achieving the goal of better, faster, cheaper, and lighter small satellites by reducing the design-load and vibration-test specifications for on-board components. In this study, a three-axis passive launch-vibration isolation sys...

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Bibliographic Details
Main Authors: Yeon-Hyeok Park, Seong-Cheol Kwon, Kyung-Rae Koo, Hyun-Ung Oh
Format: Article
Language:English
Published: MDPI AG 2021-07-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/8/8/201