Deployment Study of a Self-Rigidizable Inflatable Boom
Deployment dynamic behavior of an inflatable space structure is analyzed using a combination of gas dynamic analysis and rigid-body kinematics simulations. Modeling technique is presented for deployment of a simple cantilever boom that is rolled up on a cylindrical mandrel. During this deployment pr...
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Veröffentlicht in: | Journal of spacecraft and rockets 2006-01, Vol.43 (1), p.25-30 |
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Hauptverfasser: | , , |
Format: | Artikel |
Sprache: | eng |
Online-Zugang: | Volltext |
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Zusammenfassung: | Deployment dynamic behavior of an inflatable space structure is analyzed using a combination of gas dynamic analysis and rigid-body kinematics simulations. Modeling technique is presented for deployment of a simple cantilever boom that is rolled up on a cylindrical mandrel. During this deployment process, boom vibration is captured with the analytical models. The deployment process of a 5-m inflatable/self-rigidizable boom has also been tested, and the test results correlated very well with analytical simulations. |
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ISSN: | 0022-4650 1533-6794 |
DOI: | 10.2514/1.3283 |