3 edition of direct-interface, fusible heat sink for astronaut cooling found in the catalog.
direct-interface, fusible heat sink for astronaut cooling
by National Aeronautics and Space Administration, Ames Research Center, For sale by the National Technical Information Service in Moffett Field, Calif, [Springfield, Va
Written in English
|Other titles||Direct interface, fusible heat sink for astronaut cooling.|
|Statement||Curtis Lomax and B.W. Webbon.|
|Series||NASA technical memorandum -- 102835.|
|Contributions||Webbon, B. W., Ames Research Center.|
|The Physical Object|
|Pagination||12 p. :|
|Number of Pages||12|
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The inherent difficulties in a direct-interface heat sink have been overcome, i.e., (1) establishing an initial flow path, (2) avoiding low-flow freeze-up, and (3) achieving adequate heat-transfer. Get this from a library. A direct-interface, fusible heat sink for astronaut cooling.
[Curtis Lomax; B W Webbon; Ames Research Center.]. Curtis Lomax has written: 'A direct-interface, fusible heat sink for astronaut cooling' -- subject(s): Cooling, Extravehicular space suits, Heat transfer, Space stations, Cooling systems, Life.
Full text of "NASA Technical Reports Server (NTRS) Research and technology, " See other formats. Full text of "NASA Technical Reports Server (NTRS) NASA Tech Briefs, September Vol No.9" See other formats. A direct-interface, fusible heat sink for astronaut cooling.
NASA Technical Reports Server (NTRS) Lomax, Curtis; Webbon, B. Astronaut cooling during extravehicular activity is a critical design issue in developing a portable life support system that meets the requirements of a .