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dc.contributor.authorMorgan, Adam S. A.
dc.date.accessioned2021-03-25T18:40:26Z
dc.date.available2021-03-25T18:40:26Z
dc.date.issued2019-05-10
dc.identifieroksd_morgan_HT_2019
dc.identifier.urihttps://hdl.handle.net/11244/329057
dc.description.abstractAn analog ground test system for an inflatable crewlock was developed to facilitate deployment and training objectives during NASA Lunar Gateway ground testing and training. The result is called STARGATE, a linearly deploying structure which expands from a collapsed state in order to accomplish the deployment and demonstration objective and is capable of supporting a crew of four individuals, their equipment, and other systems to accomplished crewed testing and operations objectives. This report describes the design criteria in detail, and provides an operations manual, technical information, and design documentation.
dc.formatapplication/pdf
dc.languageen_US
dc.relationoksd_bennett_HT_2019.pdf
dc.relationoksd_jandreau_HT_2019.pdf
dc.relationoksd_white_HT_2019.pdf
dc.rightsCopyright is held by the author who has granted the Oklahoma State University Library the non-exclusive right to share this material in its institutional repository. Contact Digital Library Services at lib-dls@okstate.edu or 405-744-9161 for the permission policy on the use, reproduction or distribution of this material.
dc.titleX-Hab 2018-2019 Innovation Challenge: STARGATE inflatable crew lock: Honors thesis report
osu.filenameoksd_morgan_HT_2019.pdf
osu.accesstypeOpen Access
dc.type.genreHonors Thesis
dc.type.materialText
dc.type.materialImage
thesis.degree.disciplineMechanical and Aerospace Engineering
thesis.degree.grantorOklahoma State University


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