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dc.contributor.authorIshimatsu, Takuto
dc.contributor.authorLeveson, Nancy G.
dc.contributor.authorThomas, John P.
dc.contributor.authorKatahira, Masafumi
dc.contributor.authorMiyamoto, Yuko
dc.contributor.authorUjiie, Ryo
dc.contributor.authorNakao, Haruka
dc.contributor.authorHoshino, Nobuyuki
dc.contributor.authorFleming, Cody Harrison
dc.date.accessioned2015-05-12T16:51:38Z
dc.date.available2015-05-12T16:51:38Z
dc.date.issued2014-02
dc.date.submitted2012-10
dc.identifier.issn0022-4650
dc.identifier.issn1533-6794
dc.identifier.urihttp://hdl.handle.net/1721.1/96964
dc.description.abstractA new hazard analysis technique, called systems-theoretic process analysis, is capable of identifying potential hazardous design flaws, including software and system design errors and unsafe interactions among multiple system components. Detailed procedures for performing the hazard analysis were developed, and the feasibility and utility of using it on complex systems was demonstrated by applying it to the Japanese Aerospace Exploration Agency H-II Transfer Vehicle. In a comparison of the results of this new hazard analysis technique to those of the standard fault tree analysis used in the design and certification of the H-II Transfer Vehicle, systems-theoretic hazard analysis found all the hazardous scenarios identified in the fault tree analysis as well as additional causal factors that had not been identified by fault tree analysis.en_US
dc.description.sponsorshipJapan Manned Space Systems Corporationen_US
dc.language.isoen_US
dc.publisherAmerican Institute of Aeronautics and Astronauticsen_US
dc.relation.isversionofhttp://dx.doi.org/10.2514/1.a32449en_US
dc.rightsCreative Commons Attribution-Noncommercial-Share Alikeen_US
dc.rights.urihttp://creativecommons.org/licenses/by-nc-sa/4.0/en_US
dc.sourceMIT web domainen_US
dc.titleHazard Analysis of Complex Spacecraft Using Systems-Theoretic Process Analysisen_US
dc.typeArticleen_US
dc.identifier.citationIshimatsu, Takuto, Nancy G. Leveson, John P. Thomas, Cody H. Fleming, Masafumi Katahira, Yuko Miyamoto, Ryo Ujiie, Haruka Nakao, and Nobuyuki Hoshino. “Hazard Analysis of Complex Spacecraft Using Systems-Theoretic Process Analysis.” Journal of Spacecraft and Rockets 51, no. 2 (March 2014): 509–522.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronauticsen_US
dc.contributor.departmentMassachusetts Institute of Technology. Engineering Systems Divisionen_US
dc.contributor.mitauthorIshimatsu, Takutoen_US
dc.contributor.mitauthorLeveson, Nancy G.en_US
dc.contributor.mitauthorThomas, John P.en_US
dc.contributor.mitauthorFleming, Cody Harrisonen_US
dc.relation.journalJournal of Spacecraft and Rocketsen_US
dc.eprint.versionAuthor's final manuscripten_US
dc.type.urihttp://purl.org/eprint/type/JournalArticleen_US
eprint.statushttp://purl.org/eprint/status/PeerRevieweden_US
dspace.orderedauthorsIshimatsu, Takuto; Leveson, Nancy G.; Thomas, John P.; Fleming, Cody H.; Katahira, Masafumi; Miyamoto, Yuko; Ujiie, Ryo; Nakao, Haruka; Hoshino, Nobuyukien_US
dc.identifier.orcidhttps://orcid.org/0000-0001-6335-471X
dc.identifier.orcidhttps://orcid.org/0000-0001-6294-8890
mit.licenseOPEN_ACCESS_POLICYen_US
mit.metadata.statusComplete


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