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Hamilton Sundstrand Space Systems International (HSSSI) has been conducting an internal research and development study of an integrated portable life support system design for advanced exploration missions. This design combines several new subsystem and component concepts to achieve dramatic reductions in system weight and consumables and increased reliability and safety. The study includes the design and manufacture of subsystems and components and the assembly and test of an integrated bench top system prototype. The system design and the results of testing and analysis are described.

Hamilton Standard has been working on one EVA system concept which responds to NASA's design reference mission for the manned exploration of Mars early in the 21st century. Our concept uses a robotic support cart, to allow a simpler and lighter space suit and life support system. This, together with use of Martian resources, has shown the potential to satisfy mission needs. Present work includes preliminary design studies, analyses, and fabrication of a functional mock-up including the pressure garment, life support system, suit donning stand, and support cart. This paper describes our EVA system concept, the results of preliminary design analyses, and mock-up system tests, as well as some of the issues and challenges involved..

A fresh look at the use of astronaut time to conduct and support Extravehicular Activity (EVA) can help guide the evolution of next generation EVA systems. Studies have shown that less than 20% of the flight crew time for EVA (prior/during/post) is currently spent directly on productive tasks. In the future, longer missions, larger and more complex orbiting platforms and on-orbit maintenance of EVA equipment will drive this percentage even lower. Study of where the remaining 80% of the flight crew time presently goes indicates where improvements could be aggressively pursued for next generation systems. With the high cost per manhour on orbit, and estimated needs for 200 or more crew hours of EVA annually for space station, these improvements are clearly worthwhile. Current use of crew time before, during and after EVA were analyzed, and major uses of time identified.

With the advent of manned spacecraft opportunities requiring routine and complex extravehicular activities (EVA) a new concept for heat rejection is mandatory in order to realize maximum crewmember productivity. An optimum extravehicular mobility unit (EMU) thermal control system must be capable of successful operation without requiring expendables and without introducing contaminants into the environment, and be readily regenerable. This paper presents a regenerable non-venting thermal control subsystem requirements specification generated for a Shuttle-related EMU, identifies candidate concepts capable of fulfilling the requirements for each thermal control subsystem application, evaluates each candidate concept with respect to the subsystem requirements, and selects the best approach for each requirement.