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dc.contributor.advisorNetzer, David W.
dc.contributor.authorMcFillin, James Francis Jr.
dc.dateJune 1978
dc.date.accessioned2013-02-15T23:31:43Z
dc.date.available2013-02-15T23:31:43Z
dc.date.issued1978-06
dc.identifier.urihttp://hdl.handle.net/10945/28201
dc.descriptionApproved for public release; distribution is unlimited
dc.description.abstractAn experimental investigation was conducted to determine the feasibility and practicality of the dual rocket motor concept. Cold flow studies were performed with the aid of a ground-test simulator which incorporated a telescoping booster cavity. The effects of booster cavity length, booster cavity shockdown pressure, booster/sustainer nozzle area ratios, and aft nozzle removal on thrust and performance were explored and discussed.
dc.description.urihttp://archive.org/details/experimentalinve00mcfi
dc.language.isoen_US
dc.publisherMonterey, California: U.S. Naval Postgraduate Schoolen_US
dc.rightsThis publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.
dc.subject.lcshRocket enginesen_US
dc.titleAn experimental investigation of the dual chamber rocket motoren_US
dc.typeThesisen_US
dc.contributor.corporateNaval Postgraduate School (U.S.)
dc.contributor.departmentAeronautics
dc.subject.authorrocket
dc.subject.authordual chamber
dc.subject.authorexperimental
dc.description.serviceLieutenant, United States Navy
etd.thesisdegree.nameMaster of Science in Aeronautical Engineering
etd.thesisdegree.levelMaster of Science
etd.thesisdegree.disciplineAeronautical Engineering
etd.thesisdegree.grantorNaval Postgraduate School


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