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Acceleration induced depriming and capillary rewetting of external artery heat pipes - Comparison with SHARE-II flight experimentA combined analytical and numerical model for the analysis of the deprime and reprime/rewetting characteristics of two high-capacity external artery heat pipe designs undergoing externally induced accelerations was developed using several previously derived analytical expressions. Three distinct phases of the deprime and reprime/rewetting process were analyzed: (1) the effect of longitudinal accelerations on the depriming, (2) the time required for repriming of the liquid artery once the longitudinal acceleration has been terminated, and (3) the rewetting characteristics of the circumferential wall grooves. Combining the three processes, a technique was developed allowing the prediction of the effect of external acceleration on the characteristics of the external artery heat pipes. The predictions made with this technique agreed well with the microgravity flight results.
Document ID
19930038688
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ochterbeck, J. M.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Peterson, G. P.
(Texas A & M Univ. College Station, United States)
Ungar, E. K.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 93-0282
Meeting Information
Meeting: AIAA, Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 11, 1993
End Date: January 14, 1993
Sponsors: AIAA
Accession Number
93A22685
Funding Number(s)
CONTRACT_GRANT: NAG9-511
Distribution Limits
Public
Copyright
Other

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