The focus of this paper is a comparison of ground-based solar array deployment tests with the on-orbit deployment. The discussion includes a summary of the mechanisms involved and the correlation of a dynamics model with ground based test results. Some of the unique characteristics of the mechanisms are explained through the analysis of force and angle data acquired from the test deployments. The correlated dynamics model is then used to predict the performance of the system in its flight application.
Flight Prediction for Performance of the SWAS Solar Array Deployment Mechanism
1999
pages
Report
No indication
English
British Library Conference Proceedings | 1995
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