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Freeze Tolerant Radiator for an Advanced EMUDuring an Extravehicular Activity (EVA), the astronaut s metabolic heat and the heat produced by the Portable Life Support Unit (PLSS) must be rejected. This heat load is currently rejected by a sublimator, which vents up to eight pounds of water each EVA. However, for advanced space missions of the future, water venting to space needs to be minimized because resupply impacts from earth will be prohibitive. If this heat load could be radiated to space from the PLSS, which has enough surface area to radiate most of the heat, the amount of water now vented could be greatly reduced. Unfortunately, a radiator rejects heat at a relatively constant rate, but the astronauts generate a variable heat load depending on how hard they are working. Without a way to vary the heat removal rate, the astronaut would experience cold discomfort or even frostbite. A proven method allowing a radiator to be turned-down is to sequentially allow tubes that carry the heat transfer fluid to the radiator to freeze. A drawback of current freezable radiators using this method is that they are far to heavy for use on a PLSS, because they use heavy construction to prevent the tubes from bursting as they freeze and thaw. This creates the need for a large radiator to reject most of the heat but with a lightweight tube that doesn t burst as it freezes and thaws. The new freezable radiator for the Extravehicular Mobility Unit (EMU) has features to accommodate the expansion of the radiator fluid when it freezes, and still have the high tube to fin conductance needed to minimize the number and weight of the tubes. Radiator fluid candidates are water and a propylene glycol-water mixture. This design maintains all materials within their elastic limits so that large volume changes can be achieved without breaking the tube. This concept couples this elastic expansion with an extremely lightweight, extremely high conductivity carbon fiber fin that can carry the heat needed to thaw a frozen tube. By using most of the exposed surface area of the PLSS as a radiator, the system can reject about 75% of the highest heat load, and reduce the loss of water through sublimation by a factor of four. The proposed radiator and a small water tank can be no heavier than the current system.
Document ID
20050217244
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Copeland, Robert J.
(TDA Research, Inc. Wheat Ridge, CO, United States)
Elliott, Jeannine
(TDA Research, Inc. Wheat Ridge, CO, United States)
Weislogel, Mark
(TDA Research, Inc. Wheat Ridge, CO, United States)
Date Acquired
August 23, 2013
Publication Date
January 1, 2004
Subject Category
Man/System Technology And Life Support
Meeting Information
Meeting: International Conference on Environmental Systems
Location: Colorado Springs, CO
Country: United States
Start Date: July 1, 2004
Funding Number(s)
CONTRACT_GRANT: NAS9-03052
Distribution Limits
Public
Copyright
Other

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