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dc.creatorKurwitz, Richard Cableen_US
dc.date.accessioned2012-06-07T22:49:26Z
dc.date.available2012-06-07T22:49:26Z
dc.date.created1997en_US
dc.date.issued1997
dc.identifier.urihttp://hdl.handle.net/1969.1/ETD-TAMU-1997-THESIS-K836en_US
dc.descriptionDue to the character of the original source materials and the nature of batch digitization, quality control issues may be present in this document. Please report any quality issues you encounter to digital@library.tamu.edu, referencing the URI of the item.en_US
dc.descriptionIncludes bibliographical references: p. 80-83.en_US
dc.descriptionIssued also on microfiche from Lange Micrographics.en_US
dc.description.abstractAn experimental apparatus was designed and fabricated to test a Loop Heat Pipe under varied acceleration. The experiment consisted of both flight and ground testing as well as comparisons to a model developed from models found in literature. The purpose of the work is to obtain data and compare to thermophysical model. The thermophysical model better explains the conditions of the fluid as it moves through the wick and through the interface. The model is used to evaluate approximate acceleration induced effects and startup temperature profiles in the LHP. Variable acceleration testing was done aboard NASA's KC-1 3 5 with ground testing being performed at Texas A&M's Interphase Transport Phenomena Laboratory. Results indicate that simple correlation's and models may be used to predict steady state and some transient performance of the LHP. The model is adapted from the LHP working cycle found in the patent and other literature describing the device. The predictions closely match test data for steady state operation in both the gravity assisted and gravity opposed orientations. Transient performance predictions also gave good results, but need further evaluation to validate the assumptions. Successful operation of the LHP under high gravitational acceleration and microgravity was completed with satisfactory prediction. The use of experimentally validated predictions will allow designers to use LHP's in space systems with higher confidence in expected performance.en_US
dc.format.mediumelectronicen_US
dc.format.mimetypeapplication/pdfen_US
dc.language.isoen_USen_US
dc.publisherTexas A&M Universityen_US
dc.rightsThis thesis was part of a retrospective digitization project authorized by the Texas A&M University Libraries in 2008. Copyright remains vested with the author(s). It is the user's responsibility to secure permission from the copyright holder(s) for re-use of the work beyond the provision of Fair Use.en_US
dc.subjectnuclear engineering.en_US
dc.subjectMajor nuclear engineering.en_US
dc.titleTesting of a loop heat pipe experimental apparatus under varied accelerationen_US
dc.typeThesisen_US
thesis.degree.disciplinenuclear engineeringen_US
thesis.degree.nameM.S.en_US
thesis.degree.levelMastersen_US
dc.type.genrethesis
dc.type.materialtexten_US
dc.format.digitalOriginreformatted digitalen_US


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