Curriculum Vitaes
Profile Information
- Affiliation
- Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
- Degree
- Doctor of Science(Mar, 1989, The University of Tokyo)
- Contact information
- yoshikawa.makoto
jaxa.jp - J-GLOBAL ID
- 200901037361657011
- researchmap Member ID
- 1000304540
Research Interests
6Research Areas
2Research History
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Apr, 1998 - Sep, 2003
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Apr, 1991 - Mar, 1998
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Dec, 1996 - Dec, 1997
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Apr, 1989 - Mar, 1991
Education
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Apr, 1984 - Mar, 1989
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Apr, 1980 - Mar, 1984
Committee Memberships
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Oct, 2020 - Present
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Apr, 1994 - Present
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Jan, 2013 - Mar, 2015
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Jan, 2011 - Dec, 2012
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2009 - 2011
Awards
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Nov, 2019
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Dec, 2018
Papers
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Meteoritics & Planetary Science, Nov 25, 2024Abstract Nucleosynthetic isotope variations are powerful tracers to determine genetic relationships between meteorites and planetary bodies. They can help to link material collected by space missions to known meteorite groups. The Hayabusa 2 mission returned samples from the Cb‐type asteroid (162173) Ryugu. The mineralogical, chemical, and isotopic characteristics of these samples show strong similarities to carbonaceous chondrites and in particular CI chondrites. The nucleosynthetic isotope compositions of Ryugu overlap with CI chondrites for several elements (e.g., Cr, Ti, Fe, and Zn). In contrast to these isotopes, which are of predominately supernovae origin, s‐process variations in Mo isotope data are similar to those of carbonaceous chondrites, but even more s‐process depleted. To further constrain the origin of this depletion and test whether this signature is also present for other s‐process elements, we report Zr isotope compositions for three bulk Ryugu samples (A0106, A0106‐A0107, C0108) collected from the Hayabusa 2 mission. The data are complemented with that of terrestrial rock reference materials, eucrites, and carbonaceous chondrites. The Ryugu samples are characterized by distinct 96Zr enrichment relative to Earth, indicative of a s‐process depletion. Such depletion is also observed for carbonaceous chondrites and eucrites, in line with previous Zr isotope work, but it is more extreme in Ryugu, as observed for Mo isotopes. Since s‐process Zr and Mo are coupled in mainstream SiC grains, these distinct s‐process variations might be due to SiC grain depletion in the analyzed materials, potentially caused by incomplete sample digestion, because the Ryugu samples were dissolved on a hotplate only to avoid high blank levels for other elements (e.g., Cr). However, local depletion of SiC grains cannot be excluded. An alternative, equally possible scenario is that aqueous alteration redistributed anomalous, s‐process‐depleted, Zr on a local scale, for example, into Ca‐phosphates or phyllosilicates.
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Science Advances, 10(39), Sep 27, 2024The isotopic compositions of samples returned from Cb-type asteroid Ryugu and Ivuna-type (CI) chondrites are distinct from other carbonaceous chondrites, which has led to the suggestion that Ryugu/CI chondrites formed in a different region of the accretion disk, possibly around the orbits of Uranus and Neptune. We show that, like for Fe, Ryugu and CI chondrites also have indistinguishable Ni isotope anomalies, which differ from those of other carbonaceous chondrites. We propose that this unique Fe and Ni isotopic composition reflects different accretion efficiencies of small FeNi metal grains among the carbonaceous chondrite parent bodies. The CI chondrites incorporated these grains more efficiently, possibly because they formed at the end of the disk’s lifetime, when planetesimal formation was also triggered by photoevaporation of the disk. Isotopic variations among carbonaceous chondrites may thus reflect fractionation of distinct dust components from a common reservoir, implying CI chondrites/Ryugu may have formed in the same region of the accretion disk as other carbonaceous chondrites.
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Nature Astronomy, Sep 25, 2024
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Nature Communications, 15 7488, Aug 29, 2024 Peer-reviewedAbstract Primordial carbon delivered to the early earth by asteroids and meteorites provided a diverse source of extraterrestrial organics from pre-existing simple organic compounds, complex solar-irradiated macromolecules, and macromolecules from extended hydrothermal processing. Surface regolith collected by the Hayabusa2 spacecraft from the carbon-rich asteroid 162173 Ryugu present a unique opportunity to untangle the sources and processing history of carbonaceous matter. Here we show carbonaceous grains in Ryugu can be classified into three main populations defined by spectral shape: Highly aromatic (HA), Alkyl-Aromatic (AA), and IOM-like (IL). These carbon populations may be related to primordial chemistry, since C and N isotopic compositions vary between the three groups. Diffuse carbon is occasionally dominated by molecular carbonate preferentially associated with coarse-grained phyllosilicate minerals. Compared to related carbonaceous meteorites, the greater diversity of organic functional chemistry in Ryugu indicate the pristine condition of these asteroid samples.
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Geochimica et Cosmochimica Acta, 379 172-183, Aug, 2024
Misc.
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(6) 121-127, Mar 30, 2007Hayabusa is a spacecraft to explore the asteroid (25143) Itokawa. The spacecraft was launched on May 9, 2003 from Uchinoura Space Center using M-V launch vehicle, and arrived at (25143) Itokawa on September 12, 2005. Hayabusa adopts an Ion Engine System (IES) for its main propulsion. From the viewpoint of navigation, an error in acceleration modeling of low thrust has a great influence on accuracy of orbit determination and prediction.
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(6) 111-114, Mar 30, 2007A differential VLBI (Very Long Baseline Interferometry) technology for deep space navigation (Delta-DOR) has been developed in recent years among major Japanese VLBI agencies such as JAXA, NICT (National Institute of Information and Communications Technology), GSI (Geographical Survey Institute) and NAOJ (National Astronomical Observatory of Japan). This technology is also being developed at ESA and China independently of NASA's original system. In order to promote the data exchanges between different agencies, standard processes and message formats for use in the Delta-DOR techniques are proposed in the CCSDS (The Consultative Committee for Space Data Systems). We introduce the main features of this standard, and discuss about the future development plans for upcoming Japanese deep space missions.
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(6) 43-48, Mar 30, 2007ASTRO-G is the successive mission of HALCA (Highly Advanced Laboratory for Communications and Astronomy), which is Space VLBI (Very Long Baseline Interferometry) mission. It will try to observe in much higher resolution than HALCA by using the phase referencing method. When we use this method, the requirement of the orbit determination accuracy is about a few cm. We are considering how to achieve this accuracy.
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(6) 35-41, Mar 30, 2007HALCA (Highly Advanced Laboratory for Communications and Astronomy) (MUSES (Mu Space Engineer Satellite)-B) is the first space VLBI (Very Long Baseline Interferometry) satellite, and precise orbit determination is required from VLBI observation mission. This paper describes the outline of MUSES-B orbit determination and evaluates the achieved precision.
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(6) 105-110, Mar 30, 2007For the purpose to improve the orbit determination in Japanese space mission, Delta(VLBI) (Very Long Baseline Interferometry) observations have been conducted for NOZOMI and HAYABUSA missions. Although, Delta(VLBI) observation data has not achieved enough contribution to improvement of orbit determination. One of the reasons is low precision of group delay observable due to the lack of signal bandwidth from spacecraft. The alternative observable phase delay has potential to measure the geometrical delay with higher precision than group delay. Though, integer number of phase ambiguity is a problem to use phase delay. In November 2005, HAYABUSA has made touch down approach to asteroid Itokawa, whose orbit has been given in good precision by measurement of other techniques. In this occasion, we could use phase delay observable by avoiding the problem of phase ambiguity. And the precision of Delta(VLBI) observation with phase delay has been tested.
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宇宙科学技術連合講演会講演集(CD-ROM), 51st, 2007
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宇宙科学技術連合講演会講演集(CD-ROM), 51st, 2007
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Abstracts for fall meeting of the Japanese Society for Planetary Science, 2007 14-14, 2007Hayabusa 2 is an asteroid sample return mission following Hayabusa mission. This mission is now under study and mission target is c-type asteroid 1999JU3. From summer 2007 to April 2008 the observation from the earth is favorable conditions. This chance of observation is the first in 8 years from discovery. About 1999JU3 we had known only spectral type until now so we had observed lightcurve of it in July 2007. As a result we have found that its rotational period is about under 6 hours. This time, we will report about information of 1999JU3 we had get until now for example the result of lightcurve from July to September and about the result of AKARI in May and so on.
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Abstracts for fall meeting of the Japanese Society for Planetary Science, 2007 13-13, 2007We are investigating next missions of Hayabusa, which is the sample return mission from Asteroid Itokawa. Itokawa is an S-type asteroid, so next targets are C or D-type asteroids or dormant comets. Such objects are important from the scientific point of view. Also we should plan new mission so that we can get much more products. In this paper, we summarize what we have discussed about our new mission to primitive bodies in the solar system.
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Abstracts for fall meeting of the Japanese Society for Planetary Science, 2007 109-109, 2007The evolution of the Earth has been much affected by asteroid and comet impacts. As known in the Tunguska impact in 1908, the impacts are also threat for the human civilization. In order to avoid such threat, the discovery and follow-up observations of asteroids and comets, especially near-earth objects (NEO), are necessity. We have been carrying out the observations of NEO in Bisei Spaceguard Center since 2000. We have discovered more than 100 asteroids, and one of which was asteroid 20826, the second largest Apollo-type asteroid. We have also contributed to derivations of accurate orbital elements of known asteroids by follow-up observations. In addition to these discoveries and follow-up observations, the observations for physical properties are also important. For example, we have started light curve observations to determine the rotational period of asteroids. In this paper, we introduce the activities of Bisei Spaceguard Center.
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Abstracts for fall meeting of the Japanese Society for Planetary Science, 2007 107-107, 2007The Hayabusa spacecraft, which was launched in May 2003, arrived at Asteroid Ito-kawa in September 2005, and it made observations of Itokawa and tried touch down in about three months.Hayabusa has four scientific instruments, that is Multi-Spectral Telescopic Imager (AMICA), Laser Altimeter (LIDAR), Near-Infrared Spectrometer (NIRS), and X-ray Fluorescence Spectrometer (XRS). The data obtained by these instruments were firstly analyzed by Hayabusa Science Team and some of the results have been pub-lished as scientific papers. At the same time, the science team was preparing to open them to the public and this work has almost been done. Therefore the science team release the data archives to public from April 24, 2007. All the scientific data that Hayabusa obtained are open to the public.The Hayabusa data archives can be accessed from the following web site:(URL) http://hayabusa.sci.isas.jaxa.jp/
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JSSE Research Report, 22(3) 53-58, 2007
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Abstracts for fall meeting of the Japanese Society for Planetary Science, 2006 7-7, 2006The observation of Asteroid Itokawa by Hayabusa spacecraft has brought us a lot of new knowledge for very small (about 500m in length) S-type asteroid. We already have started to consider next space mission to small bodies in the solar system. For the next asteroid mission, we would like to explore C-type asteroid, which is also major type in the asteroid belt. This type of asteroid is supposed to have organic matter or water more than S-type asteroid, and it is important to study the material related to life. In this paper, we present the current plan for the next exploration to asteroids. We also want to encourage many researchers to join our asteroid mission.
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Abstracts for fall meeting of the Japanese Society for Planetary Science, 2006 77-77, 2006Our sub-group of SSP (Surface Science Package) has been set up in Minorbody exploration WG. Our goal is establishment of arrangement of surface science instruments for positioning, collecting geologic context, supporting selection of sampling sites, and calibrations of orbiter instruments. Scientific goal is to collect key evidence in sedimentology/stratigraphical geology under the micro-gravity environment. We will report the current status of this sub-group
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宇宙科学技術連合講演会講演集(CD-ROM), 50th, 2006
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Aeronautical and Space Sciences Japan, 53(620) 257-264, Sep 5, 2005
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Technical report of IEICE. SANE, 105(254) 19-24, Aug 19, 2005We performed more than 30 VLBI experiments for the tracking of Japan's NOZOMI Mars probe from September 2002 until June 2003. Though the rms scatter of the group delays of VLBI data from the ISAS/JAXA R&RR results are relatively large up to several tens nanoseconds, the both results are consistent with each other. The estimated position based on the phase delays are consistent with the R&RR results less than 40 milli-are second. We perform another VLBI experiments for the tracking HAYABUSA spacecraft. Both the VLBI group delays based on range signal and R&RR results are consistent with within 10 nanoseconds. We also describe an evaluation for reducing propagation delays due to the neutral atmosphere using differential VLBI technique.
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Proceedings of the IEICE General Conference, 2005(1) "SS-10"-"SS-11", Mar 7, 2005
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宇宙科学技術連合講演会講演集(CD-ROM), 49th, 2005
Books and Other Publications
19Presentations
47-
The 56th Lunar and Planetary Science Conference, Mar 13, 2025
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PERC International symposium on Dust & Parent bodies (IDP2025), Feb 27, 2025
Teaching Experience
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Apr, 2019 - Present太陽と太陽系の科学 (放送大学)
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Apr, 2011 - Present位置天文学・天体力学 (東京大学)
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Apr, 2007 - Present宇宙科学 (玉川大学)
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Apr, 2006 - PresentSpace System Engineering 3 (The Graduate University for Advanced Studies)
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2006 - Present宇宙工学概論 (総合研究大学院大学)
Professional 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, 2027
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Grants-in-Aid for Scientific Research, Japan Society for the Promotion of Science, Apr, 2023 - Mar, 2026
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Grants-in-Aid for Scientific Research Grant-in-Aid for Scientific Research (B), Japan Society for the Promotion of Science, Apr, 2018 - Mar, 2021
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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, 2016 - Mar, 2019
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Grants-in-Aid for Scientific Research, Japan Society for the Promotion of Science, 2003 - 2006