NASA NTRS · 20060040052
Deployment study of a self-rigidizable inflatable boom
Abstract
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.
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Fang, H., Lou, M., Hah, J.. 2003-04-07. Deployment study of a self-rigidizable inflatable boom. https://ntrs.nasa.gov/citations/20060040052
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