Abstract: An ideal aerospace structure would be inexpensive, a convenient size and weight for launch, easily deployed, and provide necessary stiffness/performance. This paper examines one type of potentially inexpensive, easily ...

Abstract: Design and operational issues with respect to the use of inflatable-deployable foam-rigidized components in aerospace structures are investigated in this paper. The sample structures used in this study are fabricated from ...

Abstract: An improved model for the bending behavior of space-based inflated cylindrical shells used as load-bearing beams is developed. This model reflects the biaxial state of stress present in the beam fabric due to the combination ...