Authors: Carolina Wright
Mentors: Spencer Magleby
Insitution: Brigham Young University
In recent years there has been an increasing demand for satellites that take up less space, but can still provide a large surface area. One existing solution to fit more material into less volume is deployable systems: systems that can be stowed in small spaces and then expand to occupy a large surface area. Fitting the components of a deployable system into that small space however is where difficulties arise. Thick materials do not stow into small volumes, so thinner, lightweight materials are more desirable. These types of materials can be called “gossamer” materials, and have been used in many space applications of deployable systems. Gossamer structures solve many problems related to stowing satellites in small spaces, but another complication arises for certain applications: current approaches in gossamer technology involve much creasing and wrinkling of the membrane, and do not generate the flatness required for larger, more complex systems. This is detrimental to reflectarray applications, which require a very flat surface. This research seeks to provide a solution to stowing a membrane without creasing it, thus allowing for greater flatness once deployed. This will be done by splitting the membrane into panels, folding them over each other, and rolling it up. Rolling the membrane reduces wrinkles, but adjacent panels must be able to slide past each other. Regular folding does not allow for this movement, so this requires the development of specialized surrogate folds. Surrogate folds are hinges that are used to replace the creases in a folding pattern, so the membrane itself remains unbent. As we design these folds we will look specifically for characteristics which allow for those adjacent panels to slide side by side, as well as still fold 180 degrees. This will allow the panels to fold over each other, roll up tightly, and then be deployed while leaving the membrane free of creases or wrinkles. The results of this research will be key to developing larger deployable systems in the future. Greater precision and flatness as a result of surrogate folds will open a door for further advancements in the technology that can be used on smaller, thinner reflectarray satellites.