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
Hauptverfasser: Fang, Houfei, Lou, Michael, Hah, John
Format: Artikel
Sprache:eng
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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.
ISSN:0022-4650
1533-6794
DOI:10.2514/1.3283