Design and test of a rocket motor expansion joint

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dc.contributor.authorReiserer, Russell Lawrence
dc.contributor.authorBarden, Kenneth Perrin
dc.date.accessioned2012-03-14T17:52:14Z
dc.date.available2012-03-14T17:52:14Z
dc.date.issued1947
dc.descriptionThis thesis document was issued under the authority of another institution, not NPS. At the time it was written, a copy was added to the NPS Library collection for reasons not now known.  It has been included in the digital archive for its historical value to NPS.  Not believed to be a CIVINS (Civilian Institutions) title.en_US
dc.description.abstractIf the science of guided missiles is to continue to advance, each component part of the missile mast be perfected. This means that a satisfactory propulsive system capable of continual operation to some degree must be developed. The development of a satisfactory expansion joint for the rocket motor is one phase of this problem.en_US
dc.description.serviceLieutenant Commanderen_US
dc.description.serviceLieutenant, United States Navyen_US
dc.description.urihttp://archive.org/details/designndtestofro109456369
dc.identifier.urihttps://hdl.handle.net/10945/6369
dc.publisherCalifornia Institute of Technology
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.en_US
dc.subject.lcshAeronauticsen_US
dc.titleDesign and test of a rocket motor expansion jointen_US
dc.typeThesisen_US
dspace.entity.typePublication
etd.thesisdegree.disciplineAeronautical Engineeringen_US
etd.thesisdegree.grantorCalifornia Institute of Technologyen_US
etd.thesisdegree.levelProfessional Degreeen_US
etd.thesisdegree.nameDegree in Aeronautical Engineeringen_US
etd.verifiedyesen_US
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