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
-
May, 2015 - Present
-
May, 2013 - May, 2017
-
Jul, 2003 - Sep, 2015
Awards
7-
May, 2014
-
Mar, 2004
-
Nov, 2003
Major Papers
240-
Journal of the European Ceramic Society, 42(10) 4121-4132, Aug, 2022
-
Journal of the European Ceramic Society, 42(6) 2707-2717, Jun, 2022 Peer-reviewed
-
Acta Materialia, 229 117811-117811, May, 2022 Peer-reviewed
-
Acta Materialia, 197 235-252, Sep, 2020 Peer-reviewed
-
Materials Transactions, 61(1) 68-71, 2020 Peer-reviewed
-
Acta Materialia, 176 63-72, 2019 Peer-reviewed
-
Keikinzoku/Journal of Japan Institute of Light Metals, 67(6) 228-233, 2017 Peer-reviewed
-
INTERNATIONAL JOURNAL OF FATIGUE, 87 351-358, Jun, 2016 Peer-reviewed
-
MATERIALS TRANSACTIONS, 50(12) 2858-2864, Dec, 2009 Peer-reviewed
-
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 35(12) 1666-1671, Dec, 2008 Peer-reviewed
-
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.
-
ACTA MATERIALIA, 51(7) 1909-1922, Apr, 2003 Peer-reviewed
-
MATERIALS TRANSACTIONS, 43(7) 1647-1652, Jul, 2002 Peer-reviewed
-
ACTA MATERIALIA, 49(3) 473-486, Feb, 2001 Peer-reviewed
-
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.
-
ACTA MATERIALIA, 47(5) 1653-1660, Mar, 1999 Peer-reviewed
-
ACTA MATERIALIA, 46(12) 4153-4159, Jul, 1998 Peer-reviewed
-
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
-
Materia Japan, 44(7) 554-559, Jul 20, 2005
-
53(7) 400-404, Jul 1, 2004
-
40(8) 723-730, Aug 20, 2001 Lead author
-
Bulletin of the Japan Institute of Metals, 38(5) 429-435, 1999
Books and Other Publications
3-
Aug, 2009 (ISBN: 9784781301075)
-
Presentations
168-
宇宙科学技術連合講演会講演集(CD-ROM), 2017
-
第32回宇宙構造・材料シンポジウム:講演集録 = Proceedings of 32nd Symposium on Aerospace Structure and Materials, Dec, 2016, 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)第32回宇宙構造・材料シンポジウム(2016年12月9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: SA6000087026レポート番号: B10
-
第32回宇宙構造・材料シンポジウム:講演集録 = Proceedings of 32nd Symposium on Aerospace Structure and Materials, Dec, 2016, 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)第32回宇宙構造・材料シンポジウム(2016年12月9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: SA6000087022レポート番号: B06
-
第31回宇宙構造・材料シンポジウム:講演集録 = Proceedings of the 31st Symposium on Aerospace Structure and Materials, Dec, 2015, 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)第31回宇宙構造・材料シンポジウム(2015年12月8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: SA6000047026レポート番号: B12
-
The Proceedings of the Materials and Mechanics Conference, 2015, The Japan Society of Mechanical EngineersHypervelocity impact experiments were performed on polycarbonate plates to investigate the penetrating dynamics of hypervelocity objects. The penetration behavior was observed using an ultra-high-speed video camera. The penetrating motion of projectile is analyzed by various penetration models. The penetration behavior of an intact sphere projectile is well described by the penetration model based on the spherical cavity expansion theory.
-
第30回宇宙構造・材料シンポジウム:講演集録 = Proceedings of 30th Symposium on Aerospace Structure and Materials, Dec, 2014, 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)第30回宇宙構造・材料シンポジウム(2014年12月1日. 宇宙航空研究開発機構宇宙科学研究所 (JAXA)(ISAS)), 相模原市, 神奈川県資料番号: SA6000043025レポート番号: B11
-
Mar 31, 2014, Japan Aerospace Exploration Agency (JAXA)5th Space Debris Workshop (January 22-23, 2013, Chofu Aerospace Center, Japan Aerospace Exploration Agency (JAXA)), Chofu, Tokyo, JapanA new advanced ceramic thruster made of monolithic silicon nitride has been developed in ISAS/JAXA. In order for secure operation of a spacecraft, the reliability of the ceramic component against space debris and micrometeoroid impact has been investigated through hypervelocity impact tests. Silicon nitride plates were impacted by spheres of stainless-steel and other materials with 0.2-0.8-mm diameters in the velocity range up to 8.0 km/s using a two-stage light-gas gun. Using crater depth data under various impact conditions, the penetration equation of silicon nitride was determined. The impacted samples showed fracture patterns of three types: cratering, cratering with spallation, and perforation. These fracture patterns were well categorized by the multiple forms of the penetration equation.Physical characteristics: Original contains color illustrations
-
The Proceedings of the Materials and Mechanics Conference, 2014, The Japan Society of Mechanical EngineersHypervelocity impact experiments were performed on transparent materials, SiO_2 glass and polycarbonate, to investigate the impact-induced damage process. Stress wave propagation and damage evolution associated with hypervelocity impact were visualized using a high-speed video camera. Recorded images clearly showed how stress waves propagate and interact each other, and how damages form and propagate during hypervelocity-impact event. For examples, the interaction of the transversal wave with the longitudinal wave reflected from rear surface initiated the drastic nucleation of damage points in SiO_2 glass. In the case of polycarbonate, delamination was initiated by the interaction of the reflected rarefaction waves from both side surfaces. Such information provides a valuable insight into the fundamental understanding of the hypervelocity-impact damage process on glass, ceramics, and polymer materials.
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
-
科学研究費補助金(基盤研究(A)), 日本学術振興会, 2016 - 2018
-
Grants-in-Aid for Scientific Research, Japan Society for the Promotion of Science, 2011 - 2014
-
Grants-in-Aid for Scientific Research(基盤研究(B)), Ministry of Education, Culture, Sports, Science and Technology, 2006 - 2008
-
科学研究費補助金(萌芽研究), 文部科学省, 2004 - 2005