Freeze Tolerant Radiator for Advanced EMU

2004-01-2263

07/19/2004

Event
International Conference On Environmental Systems
Authors Abstract
Content
The current Extravehicular Mobility Unit (EMU) system provides thermal control using a sublimator to reject both the heat produced by the astronaut's metabolic activity as well as the heat produced by the Portable Life Support Unit (PLSS). This sublimator vents up to eight pounds of water each Extravehicular Activity (EVA). If this load could be radiated to space, the amount of water that would need to be sublimated could be greatly reduced. There is enough surface area on the EMU that almost all of the heat can be rejected by radiation. Radiators, however, reject heat at a relatively constant rate, while the astronaut generates heat at a variable rate. To accommodate this variable heat load, NASA is developing a new freeze tolerant radiator where the tubes can selectively freeze to “turn down” the radiator and adjust to the heat rejection requirement. This radiator design significantly reduces the amount of expendable water needed for the sublimator. This paper describes the development of this freeze tolerant radiator.
Meta TagsDetails
DOI
https://doi.org/10.4271/2004-01-2263
Pages
7
Citation
Trevino, L., Copeland, R., Elliott, J., and Weislogel, M., "Freeze Tolerant Radiator for Advanced EMU," SAE Technical Paper 2004-01-2263, 2004, https://doi.org/10.4271/2004-01-2263.
Additional Details
Publisher
Published
Jul 19, 2004
Product Code
2004-01-2263
Content Type
Technical Paper
Language
English