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Propellant tank pressurization modeling for a hybrid rocket /

Thesis (M.S.)--Rochester Institute of Technology, 2009. / Typescript. Includes bibliographical references (leaves 70-73).

Identiferoai:union.ndltd.org:OCLC/oai:xtcat.oclc.org:OCLCNo/436444730
Date January 2009
CreatorsFernandez, Margaret Mary.
Source SetsOCLC
LanguageEnglish
Detected LanguageEnglish
SourceOnline version of thesis

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