Curriculum Vitaes

Hajime Yano

  (矢野 創)

Profile Information

Affiliation
Assistant Professor, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
Assistant Professor, Graduate Institute for Advanced Studies, Space and Astronautical Science Program, The Graduate University for Advanced Studies
Guest Associate Professor, Graduate School of System Design Management, Keio University
(Concurrent)Visiting Associate Professor, Institute of Advanced Biosciences
Affiliate Associate Professor, Graduate School of Science and Engineering, Hosei University
Adjunct Lecturer, School of Engineering Department of Space Systems Engineering, Kyushu Institute of Technology
Visiting Scientist, Institute of Soldier Nanotechnologies, Massachusetts Institute of Technology
Degree
Ph.D. in Space Sciences(Oct, 1995, University of Kent at Canterbury, United Kingdom)

Researcher number
00321571
J-GLOBAL ID
200901039611171139
researchmap Member ID
1000292032

External link

Prof. Hajime Yano is a space scientist, professor, and project manager of JAXA/ISAS, Japan, who specializes in solar system exploration science and astrobiology, with an emphasis on sample return missions and space experiments. 

 

As an expert in cosmic dust studies and impact physics for over a quarter of the century, his expertise extends to observational, experimental, analytical, and theoretical works of cosmic dust and space debris, as well as planetary protection and planetary defense.  In particular, he has specialized in in-situ detection and collection of cosmic dust and ultimately sample return missions from their parent bodies such as Stardust, Hayabusa, and Hayabusa-2.

 

Hajime has contributed more than 250 refereed papers as a researcher, a co-investigator, or the principal investigator of about 20 past or ongoing space projects from Japan, Europe, and the United States including LDEF, EuReCa, HST, SFU, Nozomi, Stardust, Hayabusa, Leonid-MAC, SSSAT, IKAROS, Tanpopo, BepiColombo, Hayabusa-2, Tanpopo-2, SpaceSkin, EQUULEUS, DESTINY+, Comet Interceptor, and Gateway.   Through these projects, he has accomplished a number of pioneering works that led to major scientific discoveries and “game-changing” movements in solar system exploration.   Since 2007, Hajime holds and maintains a Project Management Professional (PMP) certification and served as Tanpopo-2 project manager.

 

In the space shuttle era, Hajime established post-flight analysis procedures of micrometeoroid and orbital debris impact signatures on retrieved spacecraft surfaces.  Microscopic analyses of several hundred impacts per spacecraft such as LDEF, EuReCa, and HST revealed their origins and formed a fundamental database for dust environment modeling in near-Earth space. The SFU post-flight analysis formed Japan’s first in-situ measurement database of meteoroids and debris.

 

In 1998-2002, Hajime and his team became the world’s first to use high-definition video imagery for astronomical research and their airborne observation onboard the Leonid MAC mission, which yielded both the faintest influx and organic and volatile spectroscopy of the Leonid meteor storm.  The Leonid MAC mission resulted in a quantum leap of meteor science as a “human mission to comets without going to space, by using the atmosphere as a large dust detector”.

 

Hajime developed and operated a number of new instruments for cosmic dust detection and collection.  The detectors include the Nozomi-MDC and DESTINY+ DDA impact-induced plasma detector/analyzer, the BepiColombo-MDM and Gateway ERSA/LVDM acoustic sensors, and the ALADDIN PVDF detectors onboard SSSAT and IKAROS as well as the CLOTH PVDF integrated within MLI thermal blankets onboard EQUULEUS.  All of them are involved in hypervelocity impact calibration experiments and simulations so Hajime has developed stable shotgun techniques for microparticle impacts with two-stage light gas guns at the University of Kent in the U.K., NASA Johnson Space Center in the U.S.A., and ISAS in Japan.    ALADDIN onboard the world’s first interplanetary solar sail IKAROS deployed a 0.54 m2 detection area of cosmic dust impacts; it is the largest dedicated dust detector in the history of solar system exploration and has yielded the finest structure of dust distribution ever between the Earth and Venus.  Hajime has also collaborated with MIT ISN to upgrade the LIPIT dust accelerator for impact calibrations of space instrumentation.  He is now the science lead of the dust impact bumper for JAXA's B1 spacecraft in the Comet Interceptor mission.

 

Intact capture of meteoroids was attempted by foil stuck or aerogel modules used on LDEF, EuReCa, Stardust, Tanpopo, and Tanpopo-2. Hajime was also involved in the development of an ice-melting dust collection device for Japan’s first Antarctic micrometeorite expedition in 1999.  He is now advancing these experiences for future mission concepts like a sample return from Saturn's ring dust and Enceladus’ icy plume as well as impact ejecta from interstellar objects.

 

Also noted is Hayabusa-1&2’s asteroid surface sampling device that resulted in the world’s first asteroid sample return from Itokawa in 2010 and the second of its kind from Ryugu in 2020.  This impact sampling technique that Hajime and his team developed is a robust system suitable for almost any unknown surface conditions of an airless solid body.  Upon the sampling attempt on Itokawa by the Hayabusa-1, Hajime and his colleagues discovered evidence of granular migration on such a small body, which revolutionized ideas of their surface activities and created a new research field of “microgravity geology”.  As future sample return missions are more inclined to organic and volatile-rich small bodies, he is also contributing in the fields of astrobiology, planetary protection, and microgravity experiments.

 

As an educator, Hajime has given a number of classes and lectures for planetary science, astronautical engineering, and project management in universities and institutes worldwide.  He has supervised dozens of Masters and Ph.D. students as well as domestic interns and international students in the field of solar system science and exploration at ISAS.

 

In the international academic community, Hajime has served leading positions in organizing numerous scientific meetings in the collaboration with COSPAR, IAA, IAU, ISTS, and space agencies.  He was the chair of the inaugural meeting of the International Primitive Body Exploration Working Group (IPEWG) in 2008 and the first Asian vice chair of the COSPAR Planetary Protection Panel (PPP) in 2014-2018.  At present, he is the IAA Academician as well as the secretary of the IAA Space Physical Science Commission.  Since 2022, he has been serving as the Chair of the COSPAR Scientific Commission-B on "Space Studies of the Earth-Moon System, Planets, and Small Bodies of the Solar System".

The main belt carbonaceous (B/Cb) asteroid 1995 WF2 is named 8906 Yano.


Awards

 47

Papers

 297
  • Hajime Yano, T Kubota, H Miyamoto, T Okada, D Scheeres, Y Takagi, K Yoshida, M Abe, S Abe, O Barnouin-Jha, A Fujiwara, S Hasegawa, T Hashimoto, M Ishiguro, M Kato, J Kawaguchi, T Mukai, J Saito, S Sasaki, M Yoshikawa
    Science (New York, N.Y.), 312(5778) 1350-3, Jun 2, 2006  Peer-reviewedLead authorCorresponding author
    After global observations of asteroid 25143 Itokawa by the Hayabusa spacecraft, we selected the smooth terrain of the Muses Sea for two touchdowns carried out on 19 and 25 November 2005 UTC for the first asteroid sample collection with an impact sampling mechanism. Here, we report initial findings about geological features, surface condition, regolith grain size, compositional variation, and constraints on the physical properties of this site by using both scientific and housekeeping data during the descent sequence of the first touchdown. Close-up images revealed the first touchdown site as a regolith field densely filled with size-sorted, millimeter- to centimeter-sized grains.
  • A Fujiwara, J Kawaguchi, DK Yeomans, M Abe, T Mukai, T Okada, J Saito, H Yano, M Yoshikawa, DJ Scheeres, O Barnouin-Jha, AF Cheng, H Demura, RW Gaskell, N Hirata, H Ikeda, T Kominato, H Miyamoto, AM Nakamura, R Nakamura, S Sasaki, K Uesugi
    SCIENCE, 312(5778) 1330-1334, Jun, 2006  Peer-reviewed
    During the interval from September through early December 2005, the Hayabusa spacecraft was in close proximity to near-Earth asteroid 25143 Itokawa, and a variety of data were taken on its shape, mass, and surface topography as well as its mineralogic and elemental abundances. The asteroid's orthogonal axes are 535, 294, and 209 meters, the mass is 3.51 x 10(10) kilograms, and the estimated bulk density is 1.9 +/- 0.13 grams per cubic centimeter. The correspondence between the smooth areas on the surface ( Muses Sea and Sagamihara) and the gravitationally low regions suggests mass movement and an effective resurfacing process by impact jolting. Itokawa is considered to be a rubble-pile body because of its low bulk density, high porosity, boulder-rich appearance, and shape. The existence of very large boulders and pillars suggests an early collisional breakup of a preexisting parent asteroid followed by a re-agglomeration into a rubble-pile object.
  • NOGUCHI T., TSUCHIYAMA A., HIRATA N., NAKAMURA R., MIYAMOTO H., DEMURA H., YANO H., NAKAMURA T., SAITO J., SASAKI S., HASHIMOTO T., KUBOTA T., ISHIGURO M., ZOLENSKY M. E.
    形の科学会誌, 21(2) 192-193, 2006  Peer-reviewed
  • Hajime Yano
    Geochimica et Cosmochimica Acta, 2006  
  • S Abe, N Ebizuka, H Murayama, K Ohtsuka, S Sugimoto, MY Yamamoto, H Yano, JU Watanabe, J Borovicka
    EARTH MOON AND PLANETS, 95(1-4) 265-277, Dec, 2005  Peer-reviewed
    Spectra of persistent meteor trains were observed at wavelength between 300 and 930 nm. Two obtained train spectra during the 1998 and 2001 Leonid meteor showers are reported here. During the 1998 Leonids, one train was detected by a photographic camera with a spectrograph covering 370 - 640 nm region. On the other hand, during the 2001 Leonids, video observations were carried out using image intensified cameras in ultraviolet (UV), visible and near infrared (near-IR) wavelengths. Temperatures in persistent trains have been measured by atmospheric O-2 A( 0,1) band at the wavelength near 864.5 nm. From a video spectrum obtained just 7 s after parent. reball's. are, a rotational temperature of 250 K at altitude of 88.0 +/- 0.5 km was estimated. We can say that the cooling time scale of train strongly depends on the initial mass of its. reball at least for Leonids. Based on cooling constant calculated from our results, we estimated a temperature of similar to 130 K as a final exothermic temperature at early stage of persistent trains.
  • T Miyachi, M Fujii, N Hasebe, M Kobayashi, G Kuraza, A Nagashima, Y Nakamura, O Okudaira, N Yamashita, K Nogami, T Iwai, S Sasaki, H Ohashi, S Hasegawa, H Yano, H Shibata, N Okada, T Tou
    JOURNAL OF APPLIED PHYSICS, 98(1) 014110.1-014110.7, Jul, 2005  Peer-reviewed
    Ferroelectric lead zirconate titanate (PZT) elements were studied by directly bombarding them with hypervelocity silver particles. The mass and velocity of these hypervelocity silver particles ranged from 1 to 80 pg and 2 to 6 km/s, respectively. This report examines the pulsed signals observed immediately after collision. The first cycle of the pulse is discussed because the information on impact is presumably recorded on the wave form. The experimental data were analyzed using the wave form that was generated immediately after collision. Consequently, the following conclusions were made: (1) the sensitivity of the element is independent of the thickness of element, (2) the pulse height is proportional to the particle momentum over the measured range, and (3) the wave form is not explicitly related to the velocity of the particles at the time of collision. The potential of a single PZT element acts as a real-time detector for hypervelocity microparticles is discussed. (c) 2005 American Institute of Physics.
  • T Miyachi, M Fujii, N Hasebe, MN Kobayashi, G Kuraza, A Nagashima, Y Nakamura, K Nogami, T Iwai, S Sasaki, K Muranaga, H Ohashi, S Hasegawa, H Yano, H Shibata, E Grun, R Srama, N Okada, T Tou
    APPLIED PHYSICS LETTERS, 86(23) 1-3, Jun, 2005  Peer-reviewed
    A response from piezoelectric lead-zirconate-titanate elements was investigated by bombarding them with hypervelocity iron particles. The observed signal form was clearly dependent on the particle velocity during collisions. The signal form exhibited oscillations for particle velocities less than 6 km/s, whereas it changed drastically into a solitary pulse above 20 km/s. This behavior was exclusively classified based on the velocity. The rise time of the solitary pulse in the output form had a good correlation with the velocity at impact. The change in the form was discussed in terms of elastic and plastic states by regarding Young's modulus as a criterion between both states. It is proposed that a single piezoelectric element has the potential to detect the velocity of particles in space. (c) 2005 American Institute of Physics.
  • T Kasuga, T Yamamoto, J Watanabe, N Ebizuka, H Kawakita, H Yano
    ASTRONOMY & ASTROPHYSICS, 435(1) 341-351, May, 2005  Peer-reviewedLast author
    High-definition TV spectra in the ultraviolet - visible region were obtained during the 2002 Leonid aircraft campaign. We analyze the spectra of the brightest fireball that appeared at 03(h)47(m)54(s) UT on Nov. 19, 2002 and identify the neutral atoms, mainly MgI, FeI, CaI, and NaI in the observed wavelengths between 300 - 650 nm. The singly ionized atomic emissions, CaII and MgII lines, also appeared in the spectrum in several epochs during the series of video frames. From analysis of the spectra, time variation in the abundances of metallic atoms, along with their electronic excitation and blackbody temperatures, were obtained assuming the Local Thermal Equilibrium (LTE) condition. Both Fe and Ca abundances relative to Mg are lower than the solar abundance, while Na is slightly higher. We found correlation between the excitation temperature and the abundance of Ca, which suggests incomplete evaporation of the Ca due to intrinsic refractoriness. A search for bands of CHON-related molecules, such as OH and CN, is not successful in the brightest fireball in this study.
  • 山田哲哉, 矢野創, 内田右武, 石井信明, 安部隆士, 稲谷芳文, 藤田和央, 柳沢俊史, 伊地智幸一
    宇宙航空研究開発機構研究開発報告 JAXA-RR-, 4(04-045) 113-126, 2005  
    Normally, reentry bodies, even if they are to be recovered, are not equipped with onboard instruments such as transponders, which are useful for real-time position monitoring of the reentry bodies during the flight. This is because the surrounding plasma generated by the aerodynamic heating makes the transponder positioning nonsense as the blackout phenomena. If we could know the trajectory during the reentry phase, even if it's not monitored in real-time, the information will be a great help for the rapid recovery. The radiation from the highly-heated reentry body during the aerodynamic heating has enough intense radiation in visible region for the detection on the ground. This paper investigates a method of optical capturing of the reentry bodies by means of the visible radiation from the bodies during the aerodynamic heating. And a result of the optical tracking actually carried out on the occasion of the reentry of the REV capsule is also presented.
  • 藤原顕, 矢野創
    日本航空宇宙学会誌, 53(620) 264-271, 2005  Peer-reviewed
  • T. Miyachi, M. Fujii, N. Hasebe, M.N. Kobayashi, G. Kuraza, A. Nagashima, Y. Nakamura, O. Okudaira, N. Yamashita, K. Nogami, T. Iwai, S. Sasaki, H. Ohashi, S. Hasegawa, H. Yano, H. Shibata, T. Tou
    Jpn. J. Appl. Phys., 44(9A)(2005), 44(9A) 6870, 2005  
  • S Abe, N Ebizuka, H Yano, J Watanabe, J Borovicka
    ASTROPHYSICAL JOURNAL, 618(2) L141-L144, Jan, 2005  Peer-reviewed
    An ultraviolet-visible spectrum between 300 and 450 nm of a cometary meteoroid that originated from 55P/Tempel-Tuttle was investigated, and its new molecules, induced by atmospheric interaction, were discovered. The spectroscopy was carried out using an intensified high-definition TV camera with a slitless reflection grating during the 2001 Leonid meteor shower over Japan. A best-fit calculation mixed with atoms and molecules confirmed the first discovery of N-2(+) B (2) Sigma(u)(+) --> X (2) Sigma(g)(+) bands in the UV meteor spectrum. The N-2(+) temperature was estimated to be 10,000 K with a low number density of 1.55 x 10(5) cm(-3). Such unexpectedly strong ultraviolet emission, in particular for N-2(+) (1, 0) at 353.4 nm, is supposed to be formed through the wide dimensions of high-temperature regions caused by a large meteoroid. Spectroscopic observations of reentry capsules will provide us with good opportunities for confirming the discovered N-2(+).
  • M. Tabata, I. Adachi, T. Fukushima, H. Kawai, H. Kishimoto, A. Kuratani, H. Nakayama, S. Nishida, T. Noguchi, K. Okudaira, Y. Tajima, H. Yano, H. Yokogawa, H. Yoshida
    2005 IEEE Nuclear Science Symposium Conference Record, Vols 1-5, 816-818, 2005  Peer-reviewed
    New production methods of silica aerogel with high and low refractive indices have been developed. A very slow shrinkage of alcogel at room temperature has made possible producing aerogel with high refractive indices of up to 1.265 without cracks. Even higher refractive indices than 1.08, the transmission length of the aerogel obtained from this technique has been measured to be about 10 to 20 mm at 400 nm wave length. A mold made of alcogel which endures shrinkage in the supercritical drying process has provided aerogel with the extremely low density of 0.009g/cm(3), which corresponds to the refractive index of 1.002. We have succeeded producing aerogel with a wide range of densities.
  • T. Miyachi, M. Fujii, N. Hasebe, G. Kuraza, K. Nogami, T. Iwai, S. Sasaki, H. Ohashi, S. Hasegawa, H. Yano, H. Shibata, E. Gruen, R. Srama, N. Okada, T. Toru
    2005 IEEE Nuclear Science Symposium Conference Record, Vols 1-5, 1 423-427, 2005  Peer-reviewed
    Hypervelocity collisions of microparticles with a lead-zirconate-titanate piezoelectric element are examined. The waveforms thus obtained depend on the velocities during collision, and are classified into three categories. In particular, the first cycle of the signal observed immediately after collision is essential to obtain information on the impact. In each category, experimental formulas that are functions of the impact velocity are established based on experimental data. It is concluded that a single piezoelectric element can potentially measure the velocity and/or momentum of hypervelocity microparticles in real time. In the abovementioned context, the new dust detectors are described.
  • T Miyachi, M Fujii, N Hasebe, MN Kobayashi, G Kuraza, A Nagashima, Y Nakamura, K Nogami, T Iwai, S Sasaki, H Ohashi, S Hasegawa, H Yano, H Shibata
    SPACE DEBRIS, 35(7) 1263-1269, 2005  Peer-reviewed
    Piezoelectric lead-zirconate-titanate (PZT) elements were Studied by directly bombarding hypervelocity silver and iron particles in the velocity range of 2-63 km/s. This report focuses on the concept of "immediately after collision". This concept was realized in the leading part of a pulsed signal that exhibited no effects due to reflection. The signal form was discussed from the viewpoint that information on impact was recorded by the waveform. The results indicated that the output amplitude was independent of the thickness of a PZT element, and that the waveform was explicitly related to the velocity at collision. Further, it appeared as an oscillating form at velocities less than 6 km/s. As the velocity increased, it gradually changed to a solitary pulse. The rise time of the single solitary waveform was linearly related to velocities above 6 km/s. The potential of a single PZT element is discussed as a real-time detector for hypervelocity microparticles. (c) 2005 Published by Elsevier Ltd on behalf of COSPAR.
  • Akira Fujiwara, Masanao Abe, Hajime Yano
    HIGHLIGHTS OF ASTRONOMY, VOL 13, 13 729-729, 2005  Peer-reviewedLast author
  • Shinsuke Abe, Noboru Ebizuka, Hajime Yano, Jun-ichi Watanabe, Jiri Borovicka
    Astrophysical Journal Letters, 618(2) L141-L144, Dec 10, 2004  Peer-reviewed
    An ultraviolet-visible spectrum between 300 and 450 nm of a cometary meteoroid that originated from 55P/Tempel-Tuttle was investigated, and its new molecules, induced by atmospheric interaction, were discovered. The spectroscopy was carried out using an intensified high-definition TV camera with a slitless reflection grating during the 2001 Leonid meteor shower over Japan. A best-fit calculation mixed with atoms and molecules confirmed the first discovery of N2+ (B-X) bands in the UV meteor spectrum. The N2+ temperature was estimated to be 10,000 K with a low number density of 1.55 x 10^5 cm-3. Such unexpectedly strong ultraviolet emission, in particular for N2+(1,0) at 353.4 nm, is supposed to be formed through the wide dimensions of high-temperature regions caused by a large meteoroid. Spectroscopic observations of reentry capsules will provide us with good opportunities for confirming the discovered N2+.
  • A Tsuchiyama, T Okazawa, T Noguchi, H Yano, T Osawa, T Nakamura, K Nakamura, T Nakano, K Uesugi, H Yasuda
    METEORITICS & PLANETARY SCIENCE, 39(8) A107-A107, Aug, 2004  Peer-reviewed
  • Toru Yada, Tomoki Nakamura, Nobuo Takaoka, Takaaki Noguchi, Kentaro Terada, Hajime Yano, Takakiyo Nakazawa, Hideyasu Kojima
    Earth, Planets and Space, 56(1) 67-79, 2004  Peer-reviewed
    The accretion rate of micrometeorites in the last glacial period was estimated from the concentrations of micrometeorites in the blue ice around the Yamato Mts. in Antarctica. The samples from this study were collected from the five sampling points (M03, K02, K11, J09 and J10) in the blue ice. The blue ice was melted and filtered, and the micrometeorites were handpicked from the collected "glacial sands". The weight of the micrometeorites in the blue ice was estimated from the abundance of recovered micrometeorites and the solar noble gas concentrations in the "residue" after handpicking. The age of the blue ice from the K area was estimated to be 27-33 kyr before present based on oxygen isotope data. The estimated accretion rate to the whole Earth ranges from 5300 × 103kg/a to 16000 × 103kg/a. However, the lower end of this range probably represents lower limits due to possible loss of solar noble gases during long residence in the glacier ice. Hence, we estimate that the accretion rate of micrometeorites 27-33 kyr before present to be in the range between (11000 ± 6600) × 103kg/a and (16000 ± 9100) × 103kg/a. These results, as well as the other estimates, suggest that the accretion rate of micrometeorites in the last glacial period was comparable to that in the present. Copyright © The Society of Geomagnetism and Earth, Planetary and Space Sciences (SGEPSS) The Seismological Society of Japan The Volcanological Society of Japan The Geodetic Society of Japan The Japanese Society for Planetary Sciences.
  • T Miyachi, N Hasebe, H Ito, T Masumura, H Okada, H Yoshioka, K Nogami, T Iwai, H Shibata, Y Hamabe, S Sasaki, S Sugita, S Hasegawa, H Yano, H Ohashi, K Muranaga, M Sato, T Tou
    SPACE DEBRIS, 34(5) 935-938, 2004  Peer-reviewed
    Piezoelectric lead-zirconate-titanate was studied by bombarding with silver particles in the mass range from 2 to 100 pg, and the velocity range from 2 to 8 km/s. Output signals were uniquely identified on impact. It was found that incident energies above 100 nJ were measured unambiguously by a single lead-zirconate-titanate element. The detector characteristics were studied with respect to incident particle energy, angular dependence and size effects. Even though we have still unknown processes inherent in this detection method, the piezoelectric element has a potential as a real-time detector, if it is well calibrated. (C) 2004 COSPAR. Published by Elsevier Ltd. All rights reserved.
  • K Okudaira, T Noguchi, T Nakamura, S Sugita, Y Sekine, H Yano
    Advances in Space Research, 34(11) 2299-2304, 2004  Peer-reviewedLast author
    Silica aerogel has been used as a capturing medium for micrometeoroids and space debris. Several previous investigations suggest that aerogel could capture hypervelocity particles macroscopically intact. However, it has not been fully evaluated whether retrieved grains retain their pristine mineralogy. This study attempts to evaluate the intact survivability of high-speed projectiles in aerogel using impact experiments. Such experiments are essential for rigorous examination or further scientific discussion on the samples of on-going and future sample return missions in which aerogels are/will be used as capturing media. We fired two kinds of micrometeoroid analog materials into aerogel with a two-stage light gas gun (2-4 km/s), serpentine and cronstedtite, which are commonly found in CM/CI, and CM chondrites, respectively. As these hydrated minerals are broken down into anhydrous ones at relatively low temperatures it is suitable for the evaluation of thermal alteration during the capturing process. The retrieved residues were examined with SEM/EDS, Synchrotron Radiation-XRD, and TEM/EDS. The SR-XRD analysis revealed that most of the volumes of residues are mineralogically unaltered. TEM observations show that one serpentine grain shot at 4 km/s has an unaltered crystalline part inside, an amorphous layer, and the outermost molten aerogel layer. One cronstedtite grain shot at 3 km/s, also examined by TEM, was found to have an unaltered interior as well as a vesiculated silicate melt layer. Image analysis revealed both mineral grains reduced their volume down to 10% of the original on average. These results suggest that it is possible to capture serpentine and cronstedtite particles; mineralogically intact with lid the aerogel. at least in the interior of each particle, below 4 km/s, in spite of their large volume loss. (C) 2004 COSPAR. Published by Elsevier Ltd. All rights reserved.
  • M Morimoto, H Yamakawa, M Yoshikawa, M Abe, H Yano
    Advances in Space Research, 34(11) 2281-2285, 2004  Peer-reviewedLast author
    As one of the potential candidates of the "post-MUSES-C" minor body exploration to be launched around 2010, we have investigated scientific justifications and feasible mission scenarios. Two mission types are focused on among many other proposed mission concepts. One is the multiple rendezvous and sample return mission to asteroids whose spectral type is already known. The other is the multiple fly-bys and sample return mission to an asteroid family. This paper reports the preliminary design results of these two proposed missions. (C) 2004 COSPAR. Published by Elsevier Ltd. All rights reserved.
  • S Abe, H Yano, N Ebizuka, M Sugimoto, T Kasuga, J Watanabe
    PUBLICATIONS OF THE ASTRONOMICAL SOCIETY OF JAPAN, 55(3) 559-565, Jun, 2003  Peer-reviewed
    During the Leonid MAC 2002 airborne mission, we carried out a wide-field TV observation of the strong activity of the Leonid meteor shower from 03h30m UT through 11h50m UT on 2002 November 19. Two narrow peaks of the storm activities were observed at around 04h03m UT and 10h49m UT, with peak influx rates (mag less than or equal to + 6.5) of 1.63 x 10(-5) km(-2) s(-1) and 1.95 x 10(-5) km(-2) s(-1), respectively. Even in the full-Moon condition, the activity level of these twin peaks were comparable to that of the storm observed in 2001 over Japan. The first peak activity generated by the 7-revolution-old dust trail (ejection in 1767) was rich in bright meteors, including the fireball-class, compared to the second peak corresponding to the 4-revolution-old dust trail (ejection in 1866). The magnitude distribution indices (-2.5 less than or equal to mag less than or equal to + 3.5) were 1.70 +/- 0.10 in the first peak (7-rev) and 2.03 +/- 0.05 in the second peak (4-rev). The correlation between the observed peaks and several theoretical predictions is discussed.
  • M Ishiguro, SM Kwon, Y Sarugaku, S Hasegawa, F Usui, S Nishiura, Y Nakada, H Yano
    ASTROPHYSICAL JOURNAL, 589(2) L101-L104, Jun, 2003  Peer-reviewedLast author
    We have succeeded in detecting a dust trail along the orbit of the short-period comet 81P/Wild 2, the target of the Stardust mission, which will fly by 81P/Wild 2 in 2004 January. This is the first discovery in optical wavelengths for which an IR counterpart ( such as from IRAS) has not been reported. The detected trail extends from the nucleus to a point 2.degrees3 (0.14 AU) back along the orbit. Its width is 9" (1.4 x 10(4) km) near the nucleus. Based on a comparison between models and the observed properties of the dust trail, it is likely that the trail is composed of dust particles with a diameter of similar to1 mm (corresponding to 0.5 mg in mass). During the flyby phase of the Stardust spacecraft, it is likely that the spacecraft will experience impacts of such large dust particles along the comet's orbit as well as from smaller grains in the cometary coma. With an impact velocity of trail particles of 6.1 km s(-1), the impact fluence of 0.5 mg trail particles onto the Stardust spacecraft will be similar to0.80 day(-1) inside the dust trail. However, the Whipple bumper shields should prevent physical disruption of the spacecraft by impacting particles of up to 1 cm in size. Thus, unless the 1 mm trail dust impacts cause severe attitude control problems for the spacecraft, they may not be critically hazardous to the mission but instead may provide a unique opportunity for the first in situ flux measurement of a comet dust trail, using the Whipple bumper shield dust flux monitors.
  • HAMANE TOSHIHIKO, KAWAKITA HIDEYO, SUZUKI BUNJI, YANO HAJIME, YOSHIDA MICHITOSHI, WATANABE JUN-ICHI
    The Institute of Space and Astronautical Science report. S.P. : Proceedings of the 2002 International Science Symposium on the Leonid Meteor Storms, 15(15) 17-22, Mar, 2003  Peer-reviewed
    We carried out spectroscopic observations of comet 55P/Tempel-Tuttle, the parentbody of the Leonid meteor stream, on 1998 January 23 and 24, using a mid-dispersion spectrographin the wavelength ranges 4700-5500Å and 5700-6500Å. We detected species such as C2, NH2 , and[OI] . To characterize the comet, we estimated the gas-production rates of C2 and NH2 relative tothat of H20 and the gas-to-dust ratio based on the Haser model. The dust color was also estimatedby the method of Jewitt & Meech (1986).The gas-production rates were Q(NH2/H20)=0.23%, Q(C2/H20) = O.10%. These values aretypical for the Borrelly class which is characterized by the depletion of C2 molecule relative tothat of the Halley class. Since about 30% of detected comets belong to the Borrelly class, comet55P/Tempel-Tuttele can not be a peculiar comet, at least from spectroscopic point of view.The gas-to-dust ratio was log(Q(H20)/Afp)= 26.7, which means this comet was gas-rich relativeto comet Halley. The dust color was roughly estimated by using continuum windows, andthe dust reddening was 9.69% per 1000Å, which was consistent with other nine comets observedby Jewitt & Meech (1986).It is plausible that comet 55P/Tempel-Tuttle is not an exotic comet at any rate, except thefact that it is the parent body of the Leonid meteor stream.
  • TOTH Juraj, YANO Hajime, PORUBCAN Vladimir
    The Institute of Space and Astronautical Science report. S.P. : Proceedings of the 2002 International Science Symposium on the Leonid Meteor Storms, 15(15) 215-222, Mar, 2003  Peer-reviewed
    Recent Leonid storms provided a possibility to verify non-random grouping of particleswithin young meteoroid stream filaments. Analysis of possible clustering of meteoroids over arandom level and results based on the High-Definition TV observation of the 1999 Leonids carriedout within the scope of the Leonid MAC campaign are presented and discussed.
  • ABE Shinsuke, YANO Hajime, EBIZUKA Noboru, KASUGA Toshihiro, SUGIMOTO Masatoshi, WATANABE Jun-ichi
    The Institute of Space and Astronautical Science report. S.P. : Proceedings of the 2002 International Science Symposium on the Leonid Meteor Storms, 15(15) 149-157, Mar, 2003  Peer-reviewed
    Cometary meteoroids are considered as one of the best candidates to have suppliedorganic compounds to the Earth in the early stage of its history. However, there had been noobservational evidence to support this hypothesis until recently. Thus we conducted spectroscopicobservations of the 2001 Leonid meteor shower by using intensified HDTV cameras equipped witha reflective grating which covers 300-700 nm wavelength range. In order to minimize the effect ofair extinction near 300 nm, the observations were performed at a high elevation, i.e., the SubaruTelescope Hawaii observatory (h=4,100 m) and Nobeyama Radio Observatory (h=1,340 m) ofNational Astronomical Observatory of Japan. Spectral features of hydroxyl radicals in the cometarymeteoroids were clearly observed. In this paper, we show the first result of detection of OH emissionfrom the ground and discuss on the origin of the discovered OH A-X (0,0) band.
  • Yano Hajime, Zolensky Michael E., Fujiwara Akira, Kushiro Ikuo
    The Institute of Space and Astronautical Science report. S.P. : The First Open Competition for the MUSES-C Asteroidal Sample Preliminary Examination Team, 16(16) 1-8, Mar, 2003  Peer-reviewedLead authorCorresponding author
    ISAS's MUSES-C mission will be launched in May 2003 and attempt the world's first asteroid sample return. The target is 1998SF36, a sub-km, S-type asteroid. In order to maximize scientific output from recovered (mostly) powder samples, in June 2007, the samples should be distributed to as many qualified researchers upon proposals from all over the world. Yet, such detailed analysis proposals must rely on general characteristics of the samples studied by the initial analysis team, MASPET. MASPET will consist of ISAS scientists, NASA and Australian Co-Is, and Japanese researchers from outsourcing institutions, most of who will be selected through the open competitions of mostly non-destructive, microanalysis techniques in respective disciplines needed during the initial analysis stage. They will work as one "all-Japan" team and are responsible for characterizing the general features of the bulk and some of major samples. They also must make acquired data available to the public, after the first results published within a year from the capsule touch-down, so that international scientists can refer them and request samples for suitable, detailed analyses accordingly. The first competition was conducted in 2000-2001 and the MUSES-C Sample Advisory Committee endorsed the final recommendation in May 2002. A total of eleven applications from a large variety of analytical disciplines was received and peer-reviewed. Nine of them received two sets of unknown test samples to demonstrate their self-claimed analytical performance. Multiple international referees evaluated their reports and 6 of them were recognized as qualified to join the MASPET as of 2002. These "unknown" samples were the UNSM3529 fraction of Allende (CV3) and Valdinizza (L6). The competition will be repeated once more after the spacecraft launch and the final membership of the MASPET should be decided in the late 2005, right after the spacecraft leaves the asteroid.
  • T Miyachi, N Hasebe, H Ito, T Masumura, H Okada, H Yoshioka, M Higuchi, T Matsuyama, K Nogami, T Iwai, H Shibata, Y Hamabe, S Sasaki, S Sugita, H Ohashi, S Hasegawa, H Yano, M Sato, T Tou
    JAPANESE JOURNAL OF APPLIED PHYSICS PART 1-REGULAR PAPERS SHORT NOTES & REVIEW PAPERS, 42(3) 1496-1497, Mar, 2003  Peer-reviewed
    A lead-zirconate-titanate (PZT) element was studied by bombarding silver particles in the mass range from I to 100 pg, and the velocity from 2 to 6 km/s. Output signals were uniquely identified on impact and characterized by Fourier analysis. It was found that incident energies above 100 nJ were uniquely determined by a single PZT element. We discussed its potential as a real-time detector for space dust and debris.
  • YANO Hajime, OKADA Tatsuaki, IMAMURA Takeshi
    Journal of the Robotics Society of Japan, 21(5) 462-467, 2003  Peer-reviewedLead authorCorresponding author
  • T Takano, Y Murotani, K Maki, T Toda, A Fujiwara, S Hasegawa, A Yamori, H Yano
    JOURNAL OF APPLIED PHYSICS, 92(9) 5550-5554, Nov, 2002  Peer-reviewedLast author
    Microwave emission due to hypervelocity impacts on metallic plates has been found. The targets used in the experiment are aluminum plates with various thicknesses. The projectile, a nylon cylinder with metal screw of 0.21 gm, was accelerated up to the velocity of 4 km/s; a heterodyne receiver detected the microwave at 22 GHz. The emission is a random sequence of pulses with several nanosecond width, which lasts more than 10 mus. The phenomenon seems to be dependent on the extent of target destruction through the formation of impact craters or penetration. If so, we could use the characteristics of the phenomena to better understand the mechanical destruction process. We propose several models for the cause of this microwave generation and study them on the basis of timing relation of observed events. (C) 2002 American Institute of Physics.
  • T. Miyachi, N. Hasebe, H. Ito, T. Masumura, H. Okada, H. Yoshioka, K. Nogami, T. Iwai, H. Shibata, Y. Hamabe, S. Sasaki, S. Sugita, S. Hasegawa, H. Yano, H. Ohashi, K. Muranaga, M. Sato, T. Tou
    European Space Agency, (Special Publication) ESA SP, (500) 847-849, Jul 1, 2002  Peer-reviewed
    A PZT element was studied by bombarding silver particles in the mass range from 1 to 100 pg, and the velocity from 2 to 6 km/s. Output signals were uniquely identified on impact. They were processed on Fourier analysis. We found a simple selection rule using a relationship between Fourier components to discriminate junk events. By using the selection rule, we picked up events, by which a linear relationship between impact energy and output amplitude of the element was established It was found that incident energies above 100 nJ were determined uniquely by a single PZT element.
  • Hajime Yano, Sunao Hasegawa, Masanao Abe, Akira Fujiwara
    European Space Agency, (Special Publication) ESA SP, (500) 103-106, Jul 1, 2002  Peer-reviewedCorresponding author
    Recent studies suggested that even relatively small asteroids preserve considerable amount of regolith. Yet it is still not possible to fully understand their surface conditions only from ground observation. Thus we have developed a single sampling device that suits from metal-silicate hard surfaces to regolith layers for MUSES-C, the world's first sample return mission to a near Earth object. We report its mechanism and sampling sequence, together with results of sampling efficiency tests for 1G and micro-G gravity levels. In the vacuum micro-G environment, each sampling with this device promises several hundred mg to several g of target material fragments collected.
  • Shinsuke Abe, Hajime Yano, Noboru Ebizuka, Toshihiro Kasuga, Jun Ichi Watanabe, Masatoshi Sugimoto, Noritomo Fujino, Tetsuharu Fuse, Ryosuke Ogasawara
    European Space Agency, (Special Publication) ESA SP, (500) 213-216, Jul 1, 2002  Peer-reviewed
    Spectroscopic observations of 2001 Leonid meteor storm were carried out using a intensified HDTV camera equipped with a reflective grating covering 300 - 850 nm wavelength range. Hydroxyl radical in the cometary meteoroids was observed in fireballs and persistent trains. A good knowledge of the relationship between meteor and comet or meteorite is needed for understanding of the cometary volatiles. In this paper, we show the first detection of OH A-X (0-0) emission from the ground-based meteor observation and discuss about the origin of the discovered OH.
  • 矢野 創
    天文教育, 14(3) 20-25, May, 2002  Peer-reviewedLead authorCorresponding author
  • 矢野創
    Viva Origino, 30(3) 32-32, 2002  Peer-reviewedInvitedLead authorCorresponding author
    Origins of planetary systems and life are common goals among astronomers, biologists and planetary scientists. In the context of planetary exploration, astrobiology can be defined an interdisciplinary subject which answers fp, ne and fl parameters for the Drake-Sagan equation. The new concept of habitable zones also demands better understanding of primitive bodies of the solar system while “cosmic dust” is one of the key components that relates all the evolutionary stages (from the birth to the death) of the planetary systems and terrestrial life, for both the panspermina theory and the Urey-Miller paradigm. In particular, it is essential for us to properly conduct optical and spectroscopic observations of meteor showers such as the Leonid MAC and in-situ measurement and sample return missions to minor bodies such as MUSES-C, in order to connect between ground observation data of asteroids and comets and analytical data of cosmic dust and meteorite samples. For the latter, organic and prebiotic material analyses are important for both scientific outputs and space quarantine issues. Thus the primitive body exploration program should seek more collaboration with the astrobioloy community not only within the current program but also for new missions in the coming decade.
  • 阿部新助, 矢野創, 海老塚昇, 春日敏測, 杉本雅俊, 渡部潤一
    天文月報, 95(11) 515-528, 2002  Peer-reviewed
  • T. Miyachi, N. Hasebe, H. Ito, T. Masumura, H. Okada, H. Yoshioka, K. Nogami, Y. Hamabe, T. Iwai, S. Sasaki, H. Shibata, S. Sugita, A. Fujiwara, S. Hasegawa, H. Yano, Y. Honda, M. Sato
    Proc. of the 23rd Inter. Symp. on Space Tech. and Sci., Proc. of the 23rd Inter. Symp. 1706-1710, 2002  Peer-reviewed
  • Okudaira, K, Yano, H, Noguchi, T, Nakamura, T, Sugita, S
    Proceedings of the 23rd International Symposium on Space Technology. and Science (ISTS), 2307-2311, 2002  Peer-reviewed
  • T Noguchi, H Yano, K Terada, N Imae, T Yada, T Nakamura, H Kojima
    DUST IN THE SOLAR SYSTEM AND OTHER PLANETARY SYSTEMS, 15(C) 392-395, 2002  Peer-reviewed
    The Japanese Antarctic Research Expedition (JARS) teams have started collection of unmelted and melted micrometeorites (MMs) in Antarctica since 1996. Some results of the consortium studies are: (1) relatively common occurrence of magnesiowustite (MW) in unmelted MMs, (2) coexistence of MW with low-Ca pyroxene in moderately heated MMs, and (3) evidence that MMs were formed as small particles, rather than fragments of larger bodies, within < a few Ma.
  • Y Hamabe, S Sasaki, H Ohashi, T Kawamura, K Nogami, H Yano, S Hasegawa, H Shibata
    DUST IN THE SOLAR SYSTEM AND OTHER PLANETARY SYSTEMS, 15(C) 305-308, 2002  Peer-reviewed
    This paper reports the impact craters formed by Ag microparticles impacts, comparing with the TOF-MS (Time-Of-Flight Mass Spectrometer) spectra obtained simultaneously. The TOF spectra suggested that ions were hardly produced on AI target compared to Mo and Au targets. To determine the reason for this and to select the best material that ionizes the impacting dust particles, we observed impact craters on these targets with SEM and STM. Our results suggest that the ionization depends on the materials and that the combination of target and projectile materials causes the differences of crater shape and the Ag residue distribution.
  • GA Graham, AT Kearsley, G Drolshagen, MM Grady, IP Wright, H Yano
    DUST IN THE SOLAR SYSTEM AND OTHER PLANETARY SYSTEMS, 15(C) 372-376, 2002  Peer-reviewed
    Laboratory investigations of impact residues captured on the solar cells from the Hubble Space Telescope and on insulation foils from the Space Flyer Unit demonstrate preservation of abundant and diverse micrometeoroid and space debris remnants. Micrometeoroid residues often appear as complex melts of poly-mineralic origin derived from silicates, carbonates, metals and metal sulfides. The space debris includes paint-flakes, metal alloys and possible reactor coolant, but the most abundant components are aluminium and aluminium oxide remnants from solid rocket motor operation. The impactor origins have now been compared with the theoretical flux models for Low Earth Orbit.
  • S Sasaki, E Igenbergs, R Munzenmayer, H Ohashi, G Hofschuster, W Naumann, G Farber, F Fischer, A Fujiwara, A Glasmachers, E Grun, Y Hamabe, H Iglseder, H Miyamoto, T Mukai, K Nogami, G Schwehm, H Svedhem, M Born, T Kawamura, D Klinge, K Morishige, T Naoi, R Peeks, H Yano, K Yamakoshi
    Advances in Space Research, 15(C) 176-180, 2002  Peer-reviewed
    Mars Dust Counter (MDC) is a light-weight (730g) impact-ionization dust detector on board NOZOMI, a Japanese Mars mission, which was launched on July 4th 1998. The main aim of MDC is to detect the predicted Martian dust rings / tori. It can also cover velocity-mass ranges of interplanetary and interstellar dust particles. By August 2000, MDC had detected more than 60 dust particles. In 1999, it detected five fast particles probably of interstellar origin. For five years from 1999 to 2003, NOZOMI will orbit the sun and MDC can measure interplanetary and interstellar dust between the Earth's and Mars' orbits.
  • S Hasegawa, Y Hamabe, A Fujiwara, H Yano, S Sasaki, H Ohashi, T Kawamura, K Nogami, K Kobayashi, T Iwai, H Shibata
    INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 26(1-10) 299-308, Dec, 2001  Peer-reviewed
    In-situ dust detectors have been calibrated by dust electrostatic accelerators that can accelerate projectiles to expected mass and velocity ranges of space debris and micrometeoroids. Unfortunately, In Japan, there was no such a facility dedicated to space science research until our research group was established a few years ago. Therefore, we have developed two high voltage accelerators. One is a modified 3.75MV Van do Graaff accelerator operated by High Fluence Irradiation Facility, Research Center for Nuclear Science and Technology, the University of Tokyo (HIT), and the other is a 100kV accelerator dedicated to dust experiment at the Institute of Space and Astronautical Science (ISAS). The particle velocity using the HIT Van do Graaff accelerator is higher than those reported in other accelerator facilities under the same particle mass conditions and encompasses the desired velocity range of micro-metooroid. Time-Of-Flight dust mass spectrometer and Hybrid dust detector which are under development in Japan have been investigated using HIT dust accelerators. We have also constructed a 100kV electrostatic accelerator designed for easier handling and lower cost operation which is dedicated to dust acceleration, because the HIT Van do Graaff accelerator is being used for ion beam experiments mainly. (C) 2001 Elsevier Science Ltd. All rights reserved.
  • 矢野 創
    遊・星・人 : 日本惑星科学会誌, 10(3) 138-145, Sep 25, 2001  Peer-reviewedLead authorCorresponding author
  • H Shibata, K Kobayashi, T Iwai, Y Hamabe, S Sasaki, S Hasegawa, H Yano, A Fujiwara, H Ohashi, T Kawamura, K Nogami
    RADIATION PHYSICS AND CHEMISTRY, 60(4-5) 277-282, Mar, 2001  Peer-reviewed
    A microparticle (dust) ion source has been installed in the 3.75 MV Van de Graaff electrostatic accelerator and a new beam line for microparticle experiments has been built at the HIT facility of Research Center for Nuclear Science and Technology, the University of Tokyo. Microparticle acceleration has been successful in obtaining expected velocities of 1-20 km/s or more for micron- or submicron-sized particles. Development of in situ dust detectors on board satellites and spacecraft in the expected mass and velocity range of micrometeoroids and investigation of hypervelocity impact phenomena by using time-of-flight mass spectrometry, impact Rash measurement and scanning electron microscope observation for metals, polymers and semiconductors bombarded by micron-sized particles have been started. (C) 2001 Elsevier Science Ltd. All rights reserved.
  • Terada Kentaro, Yada Toru, Kojima Hideyasu, Noguchi Takaaki, Nakamura Tomoki, Murakami Toshio, Yano Hajime, Nozaki Wataru, Nakamuta Yoshihiro, Matsumoto Noriko, Kamata Junya, Mori Takeshi, Nakai Izumi, Sasaki Miho, Itabashi Masato, Setoyanagi Takehito, Nagao Keisuke, Osawa Takahito, Hiyagon Hajime, Mizutani Sadahiro, Fukuoka Takaaki, Nogami Ken-ichi, Ohmori Rie, Ohashi Hideo
    Antarctic meteorite research, 14 89-107, Mar, 2001  Peer-reviewed
    From November 1998 to January 1999,the 39th Japanese Antarctic Research Expedition (JARE-39) undertook Japanese first large-scale collection of Antarctic micrometeorites (AMMs), with sizes larger than 10μm, at the Meteorite Ice Field around the Yamato Mountains in Antarctica (at three different locations, for a total of 24 collection sites). The number of collected AMMs larger than 40μm is estimated to be about 5000. Here we present the general characterization (i.e., micro-morphology and surface chemical composition using SEM/EDS) of ∿810 AMMs chosen from 5 of the 24 sites. Additionall...
  • Akiko M. Nakamura, Patrick Michel, Hajime Yano, Michael E. Zolensky
    Earth, Planets and Space, 53(11) 1027, 2001  
  • GA Graham, AT Kearsley, IP Wright, MM Grady, G Drolshagen, N McBride, SF Green, MJ Burchell, H Yano, R Elliot
    PROCEEDINGS OF THE THIRD EUROPEAN CONFERENCE ON SPACE DEBRIS, VOLS 1 AND 2, 473(473) 197-202, 2001  Peer-reviewed
    Determination of the frequency and importance of impacts by space debris and micrometeoroids of below 1mm in size is best achieved by examining spacecraft surfaces that have been exposed in the near-Earth orbital environment. Post-flight investigation of the returned surface not only allows the measurement of particle flux and the dimensions of individual impact features, but also the composition and origin of the impacting bodies. Impact residue analysis is inherently a difficult task, as a particle traveling at speeds of between 5 and 70 km s(-1) leaves little chemical evidence following a hypervelocity collision. Notwithstanding this difficulty, returned surfaces from a range of spacecraft, including the Long Duration Exposure Facility (LDEF), the Space Flyer Unit (SFU), the Hubble Space Telescope (HST) and Salyut 7-Kosmos 1686 station, have enabled detailed studies on the chemistry of both micrometeoroids and space debris. The development of new dedicated capture cells, e.g. aerogel, should enable even more detailed studies of the micro-particle populations in Earth orbits, and beyond.
  • T Takano, Y Murotani, T Toda, A Fujiwara, H Yano, S Hasegawa, A Yamori
    Advances in Space Research, 103 187-192, 2001  Peer-reviewed
    Microwave emission due to a hypervelocity impact has been detected using direct detection and heterodyne detection schemes. This phenomena could be used as tools to study hypervelocity impacts or to sense space debris collisions to spacecraft. The projectile is a cylinder of 1 cm diameter and 1 cm length of the polycarbonate material, and is accelerated by a rail-gun which utilizes the electromagnetic force due to the current in plasma. Obtained velocity was 6.9 km/sec.

Misc.

 489

Books and Other Publications

 30

Presentations

 505

Teaching Experience

 5

Works

 26

Research Projects

 38

Industrial Property Rights

 8

Academic Activities

 5
  • Review, evaluation
    日本学術振興会, Jul 1, 2021 - Jun 30, 2023
  • Review, evaluation
    日本学術振興会, Jul 1, 2021 - Jun 30, 2023
  • Review, evaluation
    日本学術振興会, Jul 1, 2021 - Jun 30, 2023
  • Planning/Implementing academic research
    Keck Institute for Space Studies, California Institute of Technology, USA (Keck Institute for Space Studies, California Institute of Technology, USA), Oct 24, 2022 - Apr, 2023
    Long-period comets (LPCs) and interstellar objects (ISOs) are under-explored yet fascinating targets for planetary science, planetary defense, and astrophysics. LPCs contain volatiles preserved from the formation of the solar system and sampling those pristine ices would provide key data points to constrain the temperature and chemistry of the protoplanetary disk and early solar system dynamics. ISOs are mysterious targets of which we have only identified two so far, but are predicted to be numerous. ISOs are samples of exoplanetary systems and their in-situ exploration would bring additional perspective to our understanding of the solar system formation. While fascinating, these targets also are extremely challenging to explore closely, often arriving with little lead times, with extremely high energies, and on poorly constrained trajectories. To date, no dedicated spacecraft has been sent to explore an ISO or LPC. The short detection times before solar system departure associated with ISOs are incompatible with traditional spacecraft development schedules and funding timelines. Near Earth Object (NEO) exploration and, especially, potentially hazardous asteroid (PHA) mitigation and planetary defense share similar characteristics. The short-notice of a PHA would necessitate similar technical strategies to rapidly mitigate a potential impact. This one-week KISS workshop will unite experts in small bodies science, relevant instruments, ISO and LPC design, and mission implementation to tackle some of the most challenging aspects of developing and executing a mission to an LPC, ISO, or NEO. While the community has been unable to obtain key measurement requirements for the past LPCs and ISOs that have flown near Earth, through focused study, community building, and concept development, we can work to ensure that there are no more missed opportunities in the future!
  • Review, evaluation
    日本学術振興会, Dec, 2019 - Jan, 2020

Social Activities

 2

Media Coverage

 24

Other

 7

教育内容やその他の工夫

 1
  • Date(From)
    2012/04/01
    Subjcet
    LABAM: Laboratory for Astrobiology and Astromaterial
    Summary
    研究室理念: 宇宙塵をキーワードとする宇宙探査・実験によって可能となるアストロバイオロジーと地球外物質研究を融合して、惑星系、地球型惑星、生命の起源と進化を実証的に解明することを目指すとともに、近隣の学際研究への応用・連携を通じて人類社会の持続的なフロンティア拡大に貢献する。

その他教育活動上特記すべき事項

 10
  • Date(From)
    1999/05
    Date(To)
    2003/09
    Subjcet
    文部科学省宇宙科学研究所・惑星科学研究系(本務)
    Summary
    教授: 藤原顕
    助手: 安部正真、矢野創
  • Date(From)
    2003/10
    Date(To)
    2012/03
    Subjcet
    JAXA宇宙科学研究所・太陽系科学研究系(本務)
    Summary
    助教:矢野創
  • Date(From)
    2012/04
    Subjcet
    JAXA宇宙科学研究所・学際科学研究系・宇宙生命物質科学研究室(本務)
    Summary
    助教:矢野創
    (継続中)
  • Date(From)
    2003/10
    Date(To)
    2023/03
    Subjcet
    総合研究大学院大学・物理科学研究科・宇宙科学専攻(併任)
    Summary
    助教: 矢野創
  • Date(From)
    2010/09
    Subjcet
    慶応義塾大学大学院 システムデザインマネジメント研究科(兼任)
    Summary
    特別招聘准教授: 矢野創
    (継続中)
  • Date(From)
    2016/04
    Subjcet
    法政大学大学院 理工学研究科(併任)
    Summary
    連携准教授: 矢野創
    JAXA-法政大学連携大学院協定に基づく。(継続中)
    2016-2023年は客員准教授。
  • Date(From)
    2019/04
    Subjcet
    慶応義塾大学 先端生命科学研究所(兼任)
    Summary
    訪問准教授: 矢野創
    (継続中)
  • Date(From)
    2019/04
    Subjcet
    九州工業大学 工学部宇宙システム工学科 (兼任)
    Summary
    非常勤講師:矢野創
    (継続中)
  • Date(From)
    2017/04
    Date(To)
    2020/03
    Subjcet
    東京大学大学院 工学系研究科航空宇宙工学専攻(兼任)
    Summary
    非常勤講師:矢野創
  • Date(From)
    2023/04
    Subjcet
    総合研究大学院大学・先端学術院・宇宙科学コース(併任)
    Summary
    助教:矢野創
    (継続中)

● 指導学生等の数

 6
  • Fiscal Year
    2021年度(FY2021)
    Doctoral program
    1
    Master’s program
    3
    Students under Cooperative Graduate School System
    3
    Students under Skills Acquisition System
    1
  • Fiscal Year
    2020年度(FY2020)
    Master’s program
    5
    Students under Cooperative Graduate School System
    5
    Students under Skills Acquisition System
    1
  • Fiscal Year
    2019年度(FY2019)
    Master’s program
    6
    Students under Cooperative Graduate School System
    6
    Students under Skills Acquisition System
    2
  • Fiscal Year
    2018年度(FY2018)
    Master’s program
    5
    Students under Cooperative Graduate School System
    5
    Students under Skills Acquisition System
    2
    Others
    留学生:1
  • Fiscal Year
    2022年度(FY2022)
    Doctoral program
    1
    Master’s program
    2
    Students under Cooperative Graduate School System
    2
    Students under Skills Acquisition System
    2
  • Fiscal Year
    2023年度(FY2023)
    Doctoral program
    1
    Master’s program
    3
    Students under Cooperative Graduate School System
    3
    Students under Skills Acquisition System
    3
    JSPS Research Fellowship (Young Scientists)
    1
    Others
    留学生: 1

● 指導学生の表彰・受賞

 4
  • Student Name
    芹澤遼太
    Student affiliation
    法政大学大学院(ISAS連携大学院生)
    Award
    COSPAR Student Travel Grant Award、COSPAR, 彗星サンプルリターンを目指したCNT微粒子捕集材の実験的研究と数値解析による形状設計
    Date
    2020年7月
  • Student Name
    中澤淳一郎
    Student affiliation
    総合研究大学院大学
    Award
    帝人久村奨学金授与、公益財団法人帝人奨学会
    Date
    2021年6月
  • Student Name
    中澤淳一郎
    Student affiliation
    総合研究大学院大学
    Award
    帝人久村奨学金授与、公益財団法人帝人奨学会
    Date
    2023年4月
  • Student Name
    中澤淳一郎
    Student affiliation
    総合研究大学院大学
    Award
    日本学術振興会特別研究員(DC)
    Date
    2023年4月

● 指導学生の顕著な論文

 23
  • Student name
    Shoya IWATA
    Student affiliation
    法政大学大学院(連携大学院生)
    Author(s), journal, volume number, pagination (year of publication)
    修士論文(2024)
    Title
    Smart MLI宇宙実証機の地上校正による有効性検証と地球―月圏ダスト分布計測
  • Student name
    Francesc TINTO
    Student affiliation
    仏・国際宇宙大学院(夏季インターン学生)
    Author(s), journal, volume number, pagination (year of publication)
    ISUーMSS修士論文 Individual Project Report (2002)
    Title
    Evaluation of Effects of Regolith Size Distribution on Visible Near IR Asteroid Spectroscopy
  • Student name
    Serina DINIEGA
    Student affiliation
    仏・国際宇宙大学院
    Author(s), journal, volume number, pagination (year of publication)
    ISUーMSS修士論文 Individual Project Report (2004)
    Title
    Regolith Distribution Model for Sub-kilometer Ellipsoidal Asteroids
  • Student name
    Keisuke TERAMOTO
    Student affiliation
    東京大学大学院
    Author(s), journal, volume number, pagination (year of publication)
    修士論文(2005)
    Title
    Measurements of Sound Speed in Granular Materials Simulated Regolith
  • Student name
    Kyoko OKUDAIRA
    Student affiliation
    総合研究大学院大学
    Author(s), journal, volume number, pagination (year of publication)
    博士論文(2006)
    Title
    Evaluation of Micrometeoroid Analogs Alteration on Capturing by Aerogel
  • Student name
    Teruo MAKABE
    Student affiliation
    東京大学大学院
    Author(s), journal, volume number, pagination (year of publication)
    修士論文(2007)
    Title
    The Determination of Projectile Shape for Asteroid Impact Sampling System
  • Student name
    Takayuki HIRAI
    Student affiliation
    総合研究大学院大学
    Author(s), journal, volume number, pagination (year of publication)
    博士論文(2014)
    Title
    A New Cosmic Dust Distribution Model inside the Earth’s Orbit Based on IKAROS-ALADDIN Results
  • Student name
    Hiroyuki MOCHIZUKI
    Student affiliation
    法政大学大学院(連携大学院生)
    Author(s), journal, volume number, pagination (year of publication)
    修士論文(2018)
    Title
    複層薄膜貫通型微粒子衝突センサへの信号積分回路付与による質量推定精度の向上
  • Student name
    Maximilian SOMMER
    Student affiliation
    独・シュトッツガルト大学院(JSPSサマープログラム留学生)
    Author(s), journal, volume number, pagination (year of publication)
    修士論文(2018)
    Title
    Modelling Resonant Features in the Zodiacal Cloud
  • Student name
    Ritsuko JITSUKAWA
    Student affiliation
    法政大学大学院(連携大学院生)
    Author(s), journal, volume number, pagination (year of publication)
    修士論文(2019)
    Title
    多層断熱材一体型微粒子衝突センサの性能評価
  • Student name
    Eigo ISHIKAWA
    Student affiliation
    法政大学大学院(連携大学院生)
    Author(s), journal, volume number, pagination (year of publication)
    修士論文(2019)
    Title
    小天体ランデブーミッションに向けた低中速衝突ダストの検出回路の開発
  • Student name
    Maximilian EITEL
    Student affiliation
    独・シュトッツガルト大学院
    Author(s), journal, volume number, pagination (year of publication)
    技術研修報告書(2019)
    Title
    Tanpopo Particle Impact Analysis
  • Student name
    Keita YAMAMOTO
    Student affiliation
    法政大学大学院(連携大学院生)
    Author(s), journal, volume number, pagination (year of publication)
    修士論文(2020)
    Title
    ISSに搭載されたエアロゲル捕集材による超高速微粒子衝突頻度の経年変化に及ぼす二次イジェクタと遮蔽効果の影響
  • Student name
    Shuto OIZUMI
    Student affiliation
    法政大学大学院(連携大学院生)
    Author(s), journal, volume number, pagination (year of publication)
    修士論文(2020)
    Title
    彗星ランデブーサンプルリターンを目指した垂直配向カーボンナノチューブの微粒子捕集性能の評価
  • Student name
    Haruki NAKANO
    Student affiliation
    法政大学大学院(連携大学院生)
    Author(s), journal, volume number, pagination (year of publication)
    修士論文(2020)
    Title
    圧電性薄膜センサに衝突した微粒子の質量推定のための出力信号周波数分析
  • Student name
    Kosuke KANDO
    Student affiliation
    法政大学大学院(連携大学院生)
    Author(s), journal, volume number, pagination (year of publication)
    修士論文(2021)
    Title
    宇宙科学研究に向けたレーザー励起微粒子衝突実験装置射出部の最適化
  • Student name
    Erika MINAKAMI
    Student affiliation
    法政大学大学院(連携大学院生)
    Author(s), journal, volume number, pagination (year of publication)
    修士論文(2021)
    Title
    微粒子環境モデルの更新に向けたたんぽぽ捕集パネル 構造部上の衝突痕分析
  • Student name
    Ryota SERIZAWA
    Student affiliation
    法政大学大学院(連携大学院生)
    Author(s), journal, volume number, pagination (year of publication)
    修士論文(2021)
    Title
    彗星サンプルリターンを目指したCNT微粒子捕集材の実験的研究と数値解析による形状設計
  • Student name
    Yuki TAKEDA
    Student affiliation
    法政大学大学院(連携大学院生)
    Author(s), journal, volume number, pagination (year of publication)
    修士論文(2022)
    Title
    宇宙往還した垂直配向カーボンナノチューブによる低速衝突不定形粒子の捕集
  • Student name
    Kota ISAWA
    Student affiliation
    法政大学大学院(連携大学院生)
    Author(s), journal, volume number, pagination (year of publication)
    修士論文(2022)
    Title
    エアロゲルによる宇宙固体微粒子の衝突捕集に関する実験および数値解析

● 専任大学名

 1
  • Affiliation (university)
    総合研究大学院大学(SOKENDAI)

● 所属する所内委員会

 3
  • ISAS Committee
    2006年4月 - 2019年3月 大学共同利用スペースプラズマ(現・超高速衝突実験)専門委員会・委員
  • ISAS Committee
    2016年12月 - 2018年12月 宇宙理工学合同委員会下・宇宙科学の今後20年の構想を検討する委員会・委員
  • ISAS Committee
    2023年6月ー現在 科学データ利用委員会・委員