Satellite Hardware: Stow-and-Go for Space Travel
Source abstract
Abstract
Abstract Self-deployable booms made of flexible composites have been successfully used on spacecraft and are currently being designed into future satellite missions. Structures of this type have been proposed for decades, but their use has been limited by the difficulty of predicting their behavior in zero gravity conditions. It is now possible, however, to realistically simulate the operation of such structures using FEA software and micromechanical modeling. This article explains how boom designs for satellites are being refined using simulation data and validated by physical testing.
Source: crossref · Quality: baseline
Research context
OpenAlex topics: Structural Analysis and Optimization · Spacecraft Design and Technology · Aeroelasticity and Vibration Control
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Affiliations
California Institute of Technology , Pasadena
References
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