Curriculum Vitaes
Profile Information
- Affiliation
- Professor (Program Director), Institute of Space and Astronautical Science, Japan Aerospace Exploration AgencyProfessor, The Graduate School of Engineering, The University of Tokyo
- Degree
- Ph. D(Dec, 1989, The University of Tokyo)
- Contact information
- sato
isas.jaxa.jp
- Researcher number
- 40178710
- ORCID ID
https://orcid.org/0000-0001-7397-3477
- J-GLOBAL ID
- 200901078153204966
- researchmap Member ID
- 1000144501
- External link
Research Interests
15Research Areas
4Major Research History
9-
Dec, 2019 - Present
Education
2Major Committee Memberships
7-
Apr, 2020 - Present
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May, 2015 - Present
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May, 2013 - May, 2017
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Jul, 2003 - Sep, 2015
Awards
7-
May, 2014
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Mar, 2004
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Nov, 2003
Major Papers
240-
Journal of the European Ceramic Society, 42(10) 4121-4132, Aug, 2022
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Journal of the European Ceramic Society, 42(6) 2707-2717, Jun, 2022 Peer-reviewed
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Acta Materialia, 229 117811-117811, May, 2022 Peer-reviewed
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Acta Materialia, 197 235-252, Sep, 2020 Peer-reviewed
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Materials Transactions, 61(1) 68-71, 2020 Peer-reviewed
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Acta Materialia, 176 63-72, 2019 Peer-reviewed
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Keikinzoku/Journal of Japan Institute of Light Metals, 67(6) 228-233, 2017 Peer-reviewed
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INTERNATIONAL JOURNAL OF FATIGUE, 87 351-358, Jun, 2016 Peer-reviewed
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MATERIALS TRANSACTIONS, 50(12) 2858-2864, Dec, 2009 Peer-reviewed
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INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 35(12) 1666-1671, Dec, 2008 Peer-reviewed
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Materials Transactions, 45(7) 2295-2303, 2004 Peer-reviewedComposite creep deformation was analyzed, based on a continuum plasticity representation of the matrix, in an ideal composite at high temperatures in the case of negligible interfacial diffusion and sliding. A general formula of the steady-state creep strain rate was derived for a composite consisting of an ellipsoidal rigid reinforcement and a creeping matrix with a stress exponent of one. A closed-form solution was then derived for a composite with a cylindrical reinforcement under pure shear deformation in a two-dimensional analysis. The resultant creep deformation satisfies the requirements of impotency, volume conservation and interfacial continuity. Traces of two types of edge dislocations were analytically drawn; they show that dislocations climb over the reinforcement, retaining no dislocations either in the matrix or at the interface. Also, two types of dislocations simultaneously climb up and down at any portion in the matrix through dislocation core shuffling without long-distance diffusion. Finally, it was concluded that plastically-accommodated creep is characterized by two types of dislocations that simultaneously climb over a reinforcement, generating a heterogeneous creep strain increment without long-distance diffusion.
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ACTA MATERIALIA, 51(7) 1909-1922, Apr, 2003 Peer-reviewed
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MATERIALS TRANSACTIONS, 43(7) 1647-1652, Jul, 2002 Peer-reviewed
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ACTA MATERIALIA, 49(3) 473-486, Feb, 2001 Peer-reviewed
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MATERIALS TRANSACTIONS, 45(7) 2295-2303, 2000 Peer-reviewedComposite creep deformation was analyzed, based on a continuum plasticity representation of the matrix, in an ideal composite at high temperatures in the case of negligible interfacial diffusion and sliding. A general formula of the steady-state creep strain rate was derived for a composite consisting of an ellipsoidal rigid reinforcement and a creeping matrix with a stress exponent of one. A closed-form solution was then derived for a composite with a cylindrical reinforcement under pure shear deformation in a two-dimensional analysis. The resultant creep deformation satisfies the requirements of impotency, volume conservation and interfacial continuity. Traces of two types of edge dislocations were analytically drawn; they show that dislocations climb over the reinforcement, retaining no dislocations either in the matrix or at the interface. Also, two types of dislocations simultaneously climb up and down at any portion in the matrix through dislocation core shuffling without long-distance diffusion. Finally, it was concluded that plastically-accommodated creep is characterized by two types of dislocations that simultaneously climb over a reinforcement, generating a heterogeneous creep strain increment without long-distance diffusion.
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ACTA MATERIALIA, 47(5) 1653-1660, Mar, 1999 Peer-reviewed
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ACTA MATERIALIA, 46(12) 4153-4159, Jul, 1998 Peer-reviewed
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Acta Metallurgica et Materialia, 41(6) 1759-1767, Jun, 1993 Peer-reviewed
Major Misc.
41-
チタン = Titanium Japan, 70(3) 220-225, Jul, 2022
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Materia Japan, 44(7) 554-559, Jul 20, 2005
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53(7) 400-404, Jul 1, 2004
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40(8) 723-730, Aug 20, 2001 Lead author
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Bulletin of the Japan Institute of Metals, 38(5) 429-435, 1999
Books and Other Publications
3-
Aug, 2009 (ISBN: 9784781301075)
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Presentations
168-
宇宙構造材料シンポジウム, Dec, 2021
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宇宙構造材料シンポジウム, Dec, 2021
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International Brazing and Soldering Conference (IBSC2021), Oct, 2021
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宇宙科学技術連合講演会講演集(CD-ROM), 2020
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第35回宇宙構造・材料シンポジウム:講演集録 = Proceedings of 35th Symposium on Aerospace Structure and Materials, Dec, 2019, 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)第35回宇宙構造・材料シンポジウム(2019年12月2日. 宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS)), 相模原市, 神奈川県資料番号: SA6000146020レポート番号: A-19
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第35回宇宙構造・材料シンポジウム:講演集録 = Proceedings of 35th Symposium on Aerospace Structure and Materials, Dec, 2019, 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)第35回宇宙構造・材料シンポジウム(2019年12月2日. 宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS)), 相模原市, 神奈川県資料番号: SA6000146019レポート番号: A-18
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平成30年度宇宙科学に関する室内実験シンポジウム 講演集 = Proceedings of 2019 Symposium on Laboratory Experiment for Space Science, Feb, 2019, 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)平成30年度宇宙科学に関する室内実験シンポジウム (2019年2月28日-3月1日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)相模原キャンパス), 相模原市, 神奈川県資料番号: SA6000139025
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第34回宇宙構造・材料シンポジウム:講演集録 = Proceedings of 34th Symposium on Aerospace Structure and Materials, Dec, 2018, 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)第34回宇宙構造・材料シンポジウム(2018年12月4日. 宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS)), 相模原市, 神奈川県資料番号: SA6000137019レポート番号: A18
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第34回宇宙構造・材料シンポジウム:講演集録 = Proceedings of 34th Symposium on Aerospace Structure and Materials, Dec, 2018, 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)第34回宇宙構造・材料シンポジウム(2018年12月4日. 宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS)), 相模原市, 神奈川県資料番号: SA6000137018レポート番号: A17
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The Proceedings of the Materials and Mechanics Conference, 2018, The Japan Society of Mechanical Engineers<p>Hypervelocity-impact experiments have been performed on polycarbonate to investigate the impact-induced damage process progressing inside polymer material. The damage evolution and stress-wave propagation associated with hypervelocity impact have been observed by means of the two-directional (side-view and rear-view) scattered light imaging using two ultra-high-speed cameras. The obtained time-resolved images offer the information about the three-dimensional time evolutions of not only stress wave propagation and damage development but also damage texture which is not obtained in shadow graph. Under the 4.99 km/s impact of an alumina ceramics sphere, the alumina impactor is fractured at impact moment and the lump of impactor-fragments penetrates into polycarbonate with its collapsing. The stress wave generated by the impact propagates into target and reflects on the rear surface as the rarefaction wave. This wave induces spall fracture inside polycarbonate. After some development of spall fracture, a stress wave propagates from the spall plane. Compering the side-view and rear-view images, this stress-wave generation is considered to be tensile-stress-release from the free-surface plane formed by spallation.</p>
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The Proceedings of the Materials and Mechanics Conference, 2018, The Japan Society of Mechanical Engineers<p>In this study, a series of hypervelocity impact (HVI) experiments for silica glass plate targets were conducted to evaluate the nucleation and propagation mechanisms of spall-like damage on backside of the plates by impacting a small projectile with various conditions. Backside damage nucleation and propagation behavior was observed from two directions (side-backside) simultaneously by means of in-situ scattered light imaging coupled with an ultra-high-speed video camera. spall-like damage nucleated discontinuously with any front side damages at an area on back surface which had certain relation with change of target thickness. Nucleated damage propagated radially from each point. when the expanded damages connected with each other in high energy conditions, circular spall appeared on back surface. These observation results were compared with estimated stress wave propagation behavior, and it was suggested that the impact induced transversal stress wave affect to the nucleation and propagation. It was suggested that this damage process was quite different from the spallation of metal or other ceramics materials.</p>
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宇宙科学技術連合講演会講演集(CD-ROM), 2018
Professional Memberships
6Research Projects
23-
Grants-in-Aid for Scientific Research Grant-in-Aid for Scientific Research (B), Japan Society for the Promotion of Science, Apr, 2019 - Mar, 2022
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科学研究費補助金(基盤研究(A)), 日本学術振興会, 2016 - 2018
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Grants-in-Aid for Scientific Research, Japan Society for the Promotion of Science, 2011 - 2014
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Grants-in-Aid for Scientific Research(基盤研究(B)), Ministry of Education, Culture, Sports, Science and Technology, 2006 - 2008
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科学研究費補助金(萌芽研究), 文部科学省, 2004 - 2005