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dc.contributor.authorNishikawa, Y.
dc.contributor.authorYamamoto, M.Y.
dc.contributor.authorSansom, Eleanor
dc.contributor.authorDevillepoix, Hadrien
dc.contributor.authorTowner, Martin
dc.contributor.authorHiramatsu, Y.
dc.contributor.authorKawamura, T.
dc.contributor.authorFujita, K.
dc.contributor.authorYoshikawa, M.
dc.contributor.authorIshihara, Y.
dc.contributor.authorHamama, I.
dc.contributor.authorSegawa, N.
dc.contributor.authorKakinami, Y.
dc.contributor.authorKatao, H.
dc.contributor.authorInoue, Y.
dc.contributor.authorBland, Philip
dc.date.accessioned2023-01-31T05:05:50Z
dc.date.available2023-01-31T05:05:50Z
dc.date.issued2022
dc.identifier.citationNishikawa, Y. and Yamamoto, M.Y. and Sansom, E.K. and Devillepoix, H.A.R. and Towner, M.C. and Hiramatsu, Y. and Kawamura, T. et al. 2022. Modeling of 3D trajectory of Hayabusa2 re-entry based on acoustic observations. Publications of the Astronomical Society of Japan. 74 (2): pp. 308-317.
dc.identifier.urihttp://hdl.handle.net/20.500.11937/90266
dc.identifier.doi10.1093/pasj/psab126
dc.description.abstract

On 2020 December 5 at 17:28 UTC, Japan Aerospace Exploration Agency's Hayabusa2 sample return capsule (SRC) re-entered Earth's atmosphere. The capsule passed through the atmosphere at supersonic speeds, emitting sound and light. The inaudible sound was recorded by infrasound sensors installed by Kochi University of Technology and Curtin University. Based on analysis of the recorded infrasound, the trajectory of the SRC in two cases, one with constant-velocity linear motion and the other with silent flight, could be estimated with an accuracy of 0° 5 in elevation and 1° in direction. A comparison with optical observations suggests a state of flight in which no light is emitted but sound is emitted. In this paper, we describe the method and results of the trajectory estimation.

dc.languageEnglish
dc.publisherOXFORD UNIV PRESS
dc.relation.sponsoredbyhttp://purl.org/au-research/grants/arc/DP200102073
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/
dc.subjectScience & Technology
dc.subjectPhysical Sciences
dc.subjectAstronomy & Astrophysics
dc.subjectatmospheric effects
dc.subjectinstrumentation: miscellaneous
dc.subjectmethod: observational
dc.subjectshock waves
dc.subjectspace vehicles: instruments
dc.subjectVELOCITY METEOR FALL
dc.subjectMT. SHINMOEDAKE
dc.subjectSHOCK-WAVE
dc.subjectFIREBALLS
dc.subjectRECOVERY
dc.subjectCAPSULE
dc.subjectMISSION
dc.titleModeling of 3D trajectory of Hayabusa2 re-entry based on acoustic observations
dc.typeJournal Article
dcterms.source.volume74
dcterms.source.number2
dcterms.source.startPage308
dcterms.source.endPage317
dcterms.source.issn0004-6264
dcterms.source.titlePublications of the Astronomical Society of Japan
dc.date.updated2023-01-31T05:05:49Z
curtin.departmentSchool of Earth and Planetary Sciences (EPS)
curtin.accessStatusOpen access
curtin.facultyFaculty of Science and Engineering
curtin.contributor.orcidSansom, Eleanor [0000-0003-2702-673X]
curtin.contributor.orcidDevillepoix, Hadrien [0000-0001-9226-1870]
curtin.contributor.orcidTowner, Martin [0000-0002-8240-4150]
curtin.contributor.orcidBland, Philip [0000-0002-4681-7898]
curtin.contributor.researcheridBland, Phil [M-9392-2018]
dcterms.source.eissn2053-051X
curtin.contributor.scopusauthoridSansom, Eleanor [56460192900]
curtin.contributor.scopusauthoridDevillepoix, Hadrien [56703315600]
curtin.contributor.scopusauthoridTowner, Martin [6602160346]
curtin.contributor.scopusauthoridBland, Philip [7005534334]


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