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Spinning Dissipator for Satellite Stability by Anonymous qXxLyR6etV is a document available to read on EtoBox.

This document describes a novel attitude stabilization system for earth-orbiting satellites using a spinning dissipator. The system consists of four identical wheels mounted on the ends of cruciform structure arms, which is then spun about an axis perpendicular to provide angular momentum along the spacecraft spin axis. The document analyzes the performance of this proposed stabilization unit using the parameters of the Communications Technology Satellite. The results for a specific design indicate that g

Author

Anonymous qXxLyR6etV

Language

EN