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dc.creatorStevens, Lawrence R
dc.date.accessioned2018-09-27T17:43:38Z
dc.date.available2018-09-27T17:43:38Z
dc.date.issued1967-04
dc.date.submittedApril 1967en_US
dc.identifier.urihttp://hdl.handle.net/10388/11204
dc.description.abstractThe problem of automatic roll control of a partial payload of an upper atmosphere sounding rocket is discussed. A control system is proposed for accomplishing this function which is entirely fluidic, from sensing the necessary variables to applying the required correction torques. The design of the system, excluding the output power amplifiers and actuators,is described in detail. The system is implemented in the form of a demonstration model to illustrate the design techniques. The results of experiments carried out on this model are presented and discussed.en_US
dc.titleA FLUIDIC CONTROL SYSTEM APPLIED TO ROCKET PAYLOAD ROLL CONTROLen_US
thesis.degree.departmentMechanical Engineeringen_US
thesis.degree.disciplineMechanical Engineeringen_US
thesis.degree.grantorUniversity of Saskatchewanen_US
thesis.degree.levelMastersen_US
thesis.degree.nameMaster of Science (M.Sc.)en_US
dc.type.genreThesisen_US
dc.contributor.committeeMemberWilson, J.N.


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