Shape Memory Rigidizable Inflatable (RI) Structures for Large Space Systems Applications

Abstract

°° °C and dual T g systems that have an initial low T g and can be triggered on command by heat, radiation (UV, etc.) or chemical exposure to a higher T g. It is important for the space community to understand the major differences the SMP technologies bring to large space systems. This paper will discuss current SMP materials and then examine the implication of SMP technology as it relates to large space systems and how it can enable future missions.