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dc.contributor.advisorAlan H. Epstein.en_US
dc.contributor.authorBernier, Mathieu, 1979-en_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Mechanical Engineering.en_US
dc.date.accessioned2005-09-06T21:34:52Z
dc.date.available2005-09-06T21:34:52Z
dc.date.copyright2004en_US
dc.date.issued2004en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/27068
dc.descriptionThesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2004.en_US
dc.descriptionIncludes bibliographical references (p. 113-115).en_US
dc.description.abstractBecause of its strong oxidizing properties, high density, low-toxicity and environmentally friendly decomposition products, concentrated hydrogen peroxide has regained popularity as a propellant in many rocket applications. The MEMS-based MIT micro-rocket engine is one such application where 98% liquid hydrogen peroxide and JP7 are proposed as a propellant combination. Like other micro-thrusters concepts, the MIT micro-rocket engine uses its propellants to regeneratively cool the combustion chamber and the nozzle. Although JP7 has been proven to be an effective coolant under such conditions, hydrogen peroxide becomes unstable at high temperature and may explode, thus adding a critical constraint to the cooling scheme. To address this issue, heat transfer experiments in 95 [mu]m inside diameter, 4 mm long, electrically heated stainless steel microtubes have been performed to define the stability limit and explosion condition associated with 98% hydrogen peroxide thermal decomposition. Conditions such as pressures, temperatures, heat fluxes and length scale found in the engine were replicated. Tests were conducted whereby heat transfer to the hydrogen peroxide was increased until an explosion occurred. For each test, prior to the explosion, an experimental forced convective heat transfer coefficient has been obtained and compared to standard empirical correlations. Experimental results indicate that 98% hydrogen peroxide has limited cooling capacity for a regeneratively-cooled rocket engine. Independent of pressure and mass flow, results show that a local fluid temperature of approximately 150⁰C consistently yields an explosion in stainless steel microtubes. In addition, standard macro-scale heat transfer correlations were found to significantlyen_US
dc.description.abstract(cont.) underestimate the heat transfer rates obtained experimentally. Instead, a correlation developed for forced convective heat transfer in microtubes is presented and provides a more accurate estimate.en_US
dc.description.statementofresponsibilityby Mathieu Bernier.en_US
dc.format.extent115 p.en_US
dc.format.extent5495523 bytes
dc.format.extent5509365 bytes
dc.format.mimetypeapplication/pdf
dc.format.mimetypeapplication/pdf
dc.language.isoen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsM.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission.en_US
dc.rights.urihttp://dspace.mit.edu/handle/1721.1/7582
dc.subjectMechanical Engineering.en_US
dc.titleAn experimental investigation of heat transfer to hydrogen peroxide in microtubesen_US
dc.typeThesisen_US
dc.description.degreeS.M.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Mechanical Engineering
dc.identifier.oclc56803332en_US


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