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dc.contributor.authorDemetriades, S. Ten_US
dc.date.accessioned2006-02-02T18:42:39Z
dc.date.available2006-02-02T18:42:39Z
dc.date.issued1951en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/31045
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Chemical Engineering, 1951.en_US
dc.descriptionIncludes bibliographical references (leaves 92-93).en_US
dc.description.statementofresponsibilityby S.T. Demetriades.en_US
dc.format.extentiv, 93 leavesen_US
dc.format.extent4855314 bytes
dc.format.extent4866977 bytes
dc.format.mimetypeapplication/pdf
dc.format.mimetypeapplication/pdf
dc.language.isoengen_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.subjectChemical Engineeringen_US
dc.titleEffect of chemical structure on rocket fuel impulseen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Chemical Engineering
dc.identifier.oclc30336815en_US


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