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dc.contributor.authorBurket, V. Edward
dc.date.accessioned2015-12-02T02:07:46Z
dc.date.available2015-12-02T02:07:46Z
dc.date.issued2002-08
dc.identifier.urihttp://hdl.handle.net/11122/6243
dc.descriptionThesis (M.S.) University of Alaska Fairbanks, 2002en_US
dc.description.abstractDocumentation of a comprehensive sounding rocket payload electrical system design methodology is needed by the Alaska Student Rocket Program (ASRP) in order to allow future student designers to build upon the knowledge and experience developed on previous sounding rocket missions, rather than rediscover valuable techniques that were never documented. A systems approach to sounding rocket payload design is presented and supported by a detailed presentation and analysis of the Hawkins/30.047UO 'DIONISYS' (D-region IONIzation measurement SYStem) payload design that was used to measure the D-Region ionization density at high latitudes. Fabrication techniques and test methods that ensure the payload will survive the launch environment are also presented, as well as a post-flight analysis of the successfully launched and recovered payload.en_US
dc.language.isoen_USen_US
dc.titleSounding rocket payload electrical systems designs system: a systems approach applied to the DIONISYS payloaden_US
dc.typeThesisen_US
refterms.dateFOA2020-03-05T12:12:08Z


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