Curriculum Vitaes
Profile Information
- Affiliation
- Senior Researcher, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
- Degree
- 博士(理学)(東京大学)
- ORCID ID
https://orcid.org/0000-0001-6366-2608- J-GLOBAL ID
- 200901078920834652
- researchmap Member ID
- 5000019324
Research Areas
2Research History
7-
Apr, 2016 - Sep, 2024
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Oct, 2015 - Mar, 2016
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Apr, 2005 - Sep, 2015
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Apr, 2004 - Mar, 2005
Education
3-
Apr, 1996 - Mar, 1999
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Apr, 1993 - Mar, 1995
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Apr, 1989 - Mar, 1993
Committee Memberships
2-
Apr, 2015 - Present
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Apr, 2009 - Mar, 2015
Awards
2Papers
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Icarus, Nov, 2026Certain planetary surfaces may have been wet at the time of impact cratering, and wet surfaces can significantly affect the impact process modifying the crater size and morphology. We conducted crater formation experiments onto wet sand targets with different water contents and observed that both crater size and morphology systematically changed with the target water contents. The size of impact crater formed on wet sand target changes with water content of the target, because the cohesion and coefficient of friction of wet sand change with water content as we measure them by shear test. By varying impactor size (<mml:math><mml:mi>a</mml:mi></mml:math>) and velocity (<mml:math><mml:msub><mml:mi>v</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:math>), we simulated changing normalized gravity defined as <mml:math><mml:mi>ga</mml:mi><mml:mo>/</mml:mo><mml:msup><mml:msub><mml:mi>v</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mn>2</mml:mn></mml:msup></mml:math> to establish a crater size scaling relationship for wet sand, where <mml:math><mml:mi>g</mml:mi></mml:math> is gravity. By unifying our results and previous studies, a crater size scaling relationship was established which can express the effect of water content. The results indicate that under low-gravity conditions crater size is primarily controlled by target cohesion, whereas under high-gravity conditions crater size is more strongly influenced by internal friction. Increasing water content in the target leads to an increase in target cohesion, resulting in a decrease in crater size under low-gravity conditions, whereas it decreases the coefficient of friction in the target, leading to an increase in crater size as water content increases under high-gravity conditions. The transition boundary between the regimes where crater size is dominated by cohesion and by friction changed with water content: The surface gravity at the transition boundary for a constant impact velocity and impactor size increases in three orders of magnitude from dry to wet sand. This improved scaling relationship may help to estimate crater formation mechanisms on planetary bodies with water-bearing surface or sublayers, which is important for understanding the target properties....
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Monthly Notices of the Royal Astronomical Society, Oct, 2026Carbonaceous asteroids such as Ryugu and Bennu have experienced the catastrophic disruption of their parent bodies and subsequent cratering impacts. Their internal structure resembles a rubble pile, and some of their boulders have large cracks on their surfaces. Indeed, regolith grains sampled and returned to Earth were found to have numerous cracks, some of which extended through the entire interior of the samples. In an impact, pre-existing large cracks are likely to affect subsequent disruption and fragmentation. Hence, pre-existing large cracks affect the size distribution and lifetime of these boulders, -- and thereby asteroids. However, it is unclear how exactly fracturing is influenced by pre-existing large cracks. The purpose of this study is to investigate how pre-existing large cracks influence the fragmentation of targets. We therefore conducted impact experiments on carbonaceous meteorites with and without internal cracks. A spherical alumina projectile with 1.0 mm and a glass projectile with 0.80 mm in diameter were fired into 1--2-cm-sized Allende (CV3), Murchison (CM2), and Aguas Zarcas (CM2) targets at nominal impact velocities of 2.0 and 4.0 km <inline-formula><tex-math>$\rm {s}^{-1}$</tex-math></inline-formula>, respectively. X-ray computed tomography imaging on the meteorite before impact and on the largest fragment after impact were performed. The experiments show that, for CV and CM meteorites, several of the newly exposed surfaces on the largest impact fragments were formed along pre-existing large cracks. Measurements of fragment size distributions from the disruption of CM meteorites revealed a deficiency of small fragments, potentially explaining the scarcity of fine particles on small carbonaceous asteroids....
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Icarus, 456 117135-117135, Sep, 2026The presence of water on the Moon and on asteroids that are thought to be poor in water, either because they formed inside the snow line or because they lost much of their water during differentiation, has been suggested by multiple studies; however, its form and origin remain unclear. In this study, we conducted hypervelocity impact experiments between serpentinite projectiles and steel targets. Serpentinite contains hydroxyl and simulates hydrated impactors such as primitive asteroids. The effects of impact velocity and angle on the survival and form of water delivered to the target surface were investigated using near-infrared reflectance spectroscopy and microscopic Raman spectroscopy. Reflectance spectra of projectile materials adhered to the crater surfaces suggested that, in all head-on impact experiments with velocities of 3─7 km s−1, hydroxyl pre-existing in the projectile was almost completely lost. The spectra also showed olivine absorption features at shock pressures exceeding ∼80 GPa, and the olivine Raman peaks became narrower at higher impact velocities. Based on the comparisons with results from impact experiments with anhydrous projectiles, it is suggested that molecular water can be trapped in the melt at shock pressures below ∼100 GPa. In contrast, in the oblique impact experiments conducted in this study, decomposition of projectile material was suppressed, and hydroxyl was detected in crater samples. The current results, along with comparisons to impact velocities of asteroids in the main belt and on the Moon, suggest that molecular water derived from hydrated impactors can be detectable through spectroscopic observations....
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Monthly Notices of the Royal Astronomical Society, Jul, 2026Large main-belt asteroids with visible geometric albedos below 0.1 are predominantly classified within the C- and X-complex spectroscopic classes. C-type and dark X-type asteroids typically exhibit flat to slightly negative and positive spectral slopes, respectively. They are further distinguished by the presence (for C-types) or absence (for dark X-types) of a shallow absorption feature near 1.0-1.3 μm. We serendipitously discovered that the asteroids 1093 Freda and 1390 Abastumani display spectral characteristics intermediate between these two classes, combining a positive visible-to-near-infrared spectral slope with a shallow absorption band. A search in the literature reveals additional asteroids with similar properties. The existence of such objects, spanning a continuum of spectral shapes between C- and dark X-types, may point to a common genetic origin. Their spectral behavior could be explained by the presence of cronstedtite, an Fe-rich serpentine, on their surfaces....
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Experimental Mechanics, May 5, 2026
Misc.
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(14) 513-525, Mar 27, 20156th Space Debris Workshop (December 17-19, 2014. Chofu Aerospace Center, Japan Aerospace Exploration Agency (JAXA)(CAC)), Chofu, Tokyo, JapanTo assess debris impact risk for the satellite, submillimeter debris impact damage has not been investigated enough to conduct satellite protective designing. JAXA is researching vulnerability of satellite structure materials against submillimeter debris impact, and proposing shielding methods. This report shows summary of submillimeter impact damages of honeycomb sandwich panels. The damage of the panel was investigated by hypervelocity impact experiments with the two-stage light gas gun in ISAS. Debris larger than 0.2 mm went through the panel. In oblique impact experiments, the honeycomb core acted like multi-layer bumper.Physical characteristics: Original contains color illustrations
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Impact Frequency Estimate of Micron-sized Meteoroids and Debris on Tanpopo Capture Panels on the ISS宇宙航空研究開発機構特別資料 JAXA-SP-, (14) 550-551, Mar 27, 2015Physical characteristics: Original contains color illustrations
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Proceedings of the International Astronautical Congress, IAC, 3 1964-1969, Jan 1, 2015
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日本惑星科学会秋季講演会予稿集(Web), 2015, 2015
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日本惑星科学会秋期講演会予稿集, 2014 "O12-02", Sep 10, 2014
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日本惑星科学会秋期講演会予稿集, 2014 "O12-03", Sep 10, 2014
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日本惑星科学会秋期講演会予稿集, 2014 "O11-03", Sep 10, 2014
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日本惑星科学会秋期講演会予稿集, 2014 "O11-07", Sep 10, 2014
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日本惑星科学会秋期講演会予稿集, 2014 "O11-05", Sep 10, 2014
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日本惑星科学会秋期講演会予稿集, 2014 "O8-03", Sep 10, 2014
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日本惑星科学会秋期講演会予稿集, 2014 "O11-01", Sep 10, 2014
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2014 "OS1741-1"-"OS1741-2", Jul 19, 2014We examined ejecta size distribution when aluminum alloy 2017-T4 spheres with a diameter of 3.2 mm impacted aluminum alloy 6061-T6 targets with a plane surface and a curved surface at velocities of 4 km/s. We used a two-stage light-gas gun at the Institute of Space and Astronautical Science (ISAS)/Japan Aerospace Exploration Agency (JAXA). To examine the scattering angles of the ejecta, the following was placed 50 mm in front of the target: a witness plate (150 mm × 150 mm, 2 mm in thickness) made of copper with a hole of 30 mm. The ejection behaviors of fragments were observed using a high-speed video camera. The number of ejecta when impacting on the curved surface target was more than that when impacting on the flat surface target.
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(13) 202-212, Mar 31, 20145th Space Debris Workshop (January 22-23, 2013, Chofu Aerospace Center, Japan Aerospace Exploration Agency (JAXA)), Chofu, Tokyo, JapanTo protect a satellite from space debris impact threat, a satellite designer should employ structure material which has enough protection capability against debris impact. However, for some flexible components, it is impossible to use such strong materials, for example, expandable structures and wire harnesses. To protect these flexible components, a flexible debris bumper is needed. High strength fiber fabric is one of flexible debris bumper material. Since the alamido fiber has high tensile and shear strength, the alamido fiber fabric is known to be also useful for high velocity impact protection. The alamido fiber fabric was used as a part of the Staffed Whipple Bumper installed on the International Space Station. A satellite on the low earth orbit needs to pay attention to impacts on debris smaller than 1 mm, because debris environment models show such small debris will impact on the satellite during its operation lifetime. Therefore, to employ the alamido fiber fabric as a debris bumper, it is necessary to know their sub-millimeter debris impact damage. The purpose of this study is to investigate sub-millimeter debris impact damage of the fiber fabric.Physical characteristics: Original contains color illustrations
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(13) 213-223, Mar 31, 20145th Space Debris Workshop (January 22-23, 2013, Chofu Aerospace Center, Japan Aerospace Exploration Agency (JAXA)), Chofu, Tokyo, JapanAluminum Foam targets were tested as a favored candidate material for a light-weight space debris bumper shield. A target consists of layers of aluminum foam plates, and each plate was made of aluminum powder, tens of micro-meters in diameter. Their porosity, density, and nominal diameters of pores is 82 %, 500 kg/m3, and 0.3 mm, respectively. Metal spheres are employed as simulated debris and accelerated to 4 to 7 km/sec. Bulb shaped craters with small entrance holes are observed. No high-speed ejecta is observed by use of a high-speed video camera.Physical characteristics: Original contains color illustrations
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(13) 224-232, Mar 31, 20145th 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
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Meeting abstracts of the Physical Society of Japan, 69(1) 280-280, Mar 5, 2014
Major Presentations
132Professional Memberships
3Research Projects
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科学研究費助成事業, 日本学術振興会, Apr, 2024 - Mar, 2028
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Grants-in-Aid for Scientific Research Grant-in-Aid for Scientific Research (A), Japan Society for the Promotion of Science, Apr, 2022 - Mar, 2026
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科学研究費助成事業 基盤研究(B), 日本学術振興会, Apr, 2021 - Mar, 2024
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科学研究費助成事業 基盤研究(B), 日本学術振興会, Apr, 2021 - Mar, 2024
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Grants-in-Aid for Scientific Research Grant-in-Aid for Scientific Research (C), Japan Society for the Promotion of Science, Apr, 2020 - Mar, 2023