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  • 1
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    Thermal control system technology discipline (1990)
    In:  CASI
    Details
    Publication Date: 2013-08-31
    Description: Viewgraphs on thermal control systems technology discipline for Space Station Freedom are presented. Topics covered include: heat rejection; heat acquisition and transport; monitoring and control; passive thermal control; and analysis and test verification.
    Keywords: SPACECRAFT DESIGN, TESTING AND PERFORMANCE
    Type: NASA, Washington, Technology for Space Station Evolution. Executive Summary and Overview; p 247-265
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 2
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    Forced flow evaporator for unusual gravity conditions (1987)
    In:  CASI
    Details
    Publication Date: 2019-07-12
    Description: Low efficiency heat transfer in evaporators subject to unusual gravitational conditions is avoided through the use of a spiral evaporator conduit 12 receiving at an inlet 14 a vaporizable coolant at least partly in the liquid phase. Flow of the coolant through the conduit 12 demists the coolant by centrifuging the liquid phase against a pressurre wall 44 of the conduit 12. Vapor flow 40 induces counterrotating vortices 46, 48 which circulate the liquid phase coolant around the interior of the conduit 12 to wet all surfaces thereof.
    Keywords: Fluid Mechanics and Thermodynamics
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 3
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    Forced-Flow Evaporative Cooler (1987)
    In:  Other Sources
    Details
    Publication Date: 2019-07-12
    Description: Evaporative cooler absorbs heat efficiently under unusual gravitational conditions by using centrifugal force and vapor vortexes to maintain good thermal contact between heat-transfer surface and vaporizable coolant. System useful for cooling electronic or other equipment under low gravity encountered in spacecraft or under multiple-gravity conditions frequently experienced in high-performance airplanes.
    Keywords: MACHINERY
    Type: MSC-21078 , NASA Tech Briefs (ISSN 0145-319X); 11; 6; P. 58
    Format: text
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    NASA TECHNICAL REPORTS
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