Search Results

Dust mitigation has been identified as a major obstacle to lunar and Mars surface operations for space suits, robotics, and vehicle systems. Experience from the Apollo program has demonstrated that lunar stays of limited duration will be difficult and dangerous if dramatic measures are not taken to mitigate the impacts of dust contamination. Numerous mitigation approaches have been studied in the past including electrostatic materials, cleaning techniques, and suit-locks. Many of these approaches are effective in operation but are challenged by the trend of returning to a single space suit system, similar to Apollo, which is used for launch/entry as well as surface and contingency extra-vehicular activity (EVA) operations. Bringing the surface suit inside the vehicle after surface EVA will transfer surface material in the vehicle.

This paper summarizes the development of multi-functional intelligent flexible materials for deployable space structures, otherwise known as the InFlex program. The goal of the work was to enhance the capabilities of inflatable structures for exploration activities such as habitats, airlocks, and space suits, with improved materials ultimately to reduce crew burden and lifecycle costs, improve system safety, and reduce system mass and launch volume. Several technical areas were investigated concurrently in an effort to combine functions and create efficient structures. These included self-healing materials, structural health monitoring systems, radiation protective materials, reduced permeability materials, anti-microbial materials, and embedded power generation and storage technologies. Methods of signal transfer were also studied in conjunction with a centralized display and warning system to interact with systems operations personnel.