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Capillary Two-Phase Thermal Devices for Space ApplicationsThis is the presentation file for an invited seminar for Department of Mechanical and Aerospace Engineering at the Case Western Reserve University. The seminar is scheduled for April 1, 2016.Description: This presentation will discuss operating principles and performance characteristics of heat pipes (HPs) and loop heat pipes (LHPs) and their application for spacecraft thermal control. Topics include: 1) HP operating principles; 2) HP performance characteristics; 3) LHP pressure profiles; 4) LHP operating temperature; 5) LHP operating temperature control; and 6) Examples of using HPs and LHPs on NASA flight projects.
Document ID
20160004212
Acquisition Source
Goddard Space Flight Center
Document Type
Presentation
Authors
Ku, Jentung
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Date Acquired
April 1, 2016
Publication Date
April 1, 2016
Subject Category
Fluid Mechanics And Thermodynamics
Spacecraft Design, Testing And Performance
Report/Patent Number
GSFC-E-DAA-TN30338
Report Number: GSFC-E-DAA-TN30338
Meeting Information
Meeting: Seminar - Department of Mechanical and Aerospace Engineering
Location: Cleveland, OH
Country: United States
Start Date: March 29, 2016
Sponsors: Case Western Reserve Univ.
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Thermal Contgrol
Heat Pipes
Two-Phase
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