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
  • H Yoshimi, S Sasaki, H Ohashi, T Kawamura, KI Nogami, H Yano, S Hasegawa, H Shibata
    PROCEEDINGS OF THE METEOROIDS 2001 CONFERENCE, 495(495) 621-624, 2001  Peer-reviewed
    In order to analyse the elements of dust particles in space, we have been developing a reflectron-type dust TOF-MS (Time-Of-Flight Mass Spectrometer) with a curved electric field. Now we have done performance experiments of our device by impacting hypervelocity microparticles with a Van de Graaff accelerator at HIT (High Fluence Irradiation Facility, University of Tokyo), where carbon particles of 0.3-2.0 mum in diameter are accelerated up to 5-20 km/s which are comparable with the velocity of dust particles in space. The results showed the device has higher mass resolution than the system with a parallel reflecting region under the same experiment situation by factor 2 or 3. Moreover the TOF spectra showed the higher detection efficiency, and the value was 10 times higher compared to the parallel reflectron TOF-MS. These effective results are considered to be caused by a curved electric field in a reflecting region.
  • YAMAMOTO Satoru, YANO Hajume, FUJIWARA Akira
    Planetary people, 9(4) 172-175, Dec 1, 2000  Peer-reviewed
  • T Yada, T Nakamura, T Noguchi, H Yano, K Terada, T Murakami, H Kojima
    METEORITICS & PLANETARY SCIENCE, 35 A173-A174, Sep, 2000  
  • FUJIWARA Akira, ABE Masanao, HASEGAWA Sunao, SHIMADA Takafumi, ONOSE Naom, YANO Hazime, HIGUCHI Ken, SAWAI Shuziro, KAWAGUCHI Jun-ichiro, TAKAGI Shu, TAKAGI Yasuhiko, TAKAYAMA Kazuyoshi, NONAKA Satoru, OKANO Kouichi, MIWA Chiyomi, OKUDAIRA Toshiaki, YAJIMA Satoru
    JASMA, 17(3) 178-182, Jul 31, 2000  Peer-reviewed
    Opportunities to collect test pieces from various kind of bodies in space is increasing. In this study we obtained data re­quired for design of a device which collects samples by shooting a small projectile onto the targeted bodies and concentrating ejected fragments through a funnel-shaped horn. We made a series of studies including experiments to investigate production of fragments at impact and motion of fragments reflecting inside the horn, capturing tests both in 1 G­ environment on the ground and under reduced gravity using an airplane. These investigations show that more than 40% of the ejecta from brick-like bodies can be caputured by this device.
  • 日本惑星科学会誌「遊・星・人」, 9(4) 172-226, 2000  Peer-reviewed
  • H Yano, K Morishige, SP Deshpande, Y Maekawa, S Kibe, MJ Neish, EA Taylor
    Advances in Space Research, 25(2) 293-298, 2000  Peer-reviewedLead authorCorresponding author
    170 hypervelocity impact signatures on the MLI and SSM surfaces of the SFU spacecraft were studied their three dimensional morphology and elemental analysis to discriminate them by natural origin from those by artificial debris. Ratio of meteoroids against debris, with some "unknown" and "undetermined" origins, is compared to results from previously retrieved spacecraft. those of LDEF, EuReCa and HST. The impact flux on the Sun pointing face is also compared with (C) 1999 COSPAR. Published by Elsevier Science Ltd.
  • 秋山演亮, 矢野創, 吉田二美, 安部正真, 藤原顕
    日本惑星科学会誌 遊・星・人, 9(4) 216-226, 2000  Peer-reviewed
  • JAM McDonnell, MJ Burchell, SF Green, M Leese, D Wallis, JC Zarnecki, DJ Catling, DE Brownlee, P Tsou, L Colangeli, E Bussoletti, G Drolshagen, CR Maag, H Yano
    Advances in Space Research, 25(2) 315-322, 2000  Peer-reviewedLast author
    The capabilities of combining Aerogel (A) as a passive target and position-sensitive impact sensing (PSIS) are examined; experimental performance factors are established from tests on Hypervelocity Impact Facilities at the University of Kent and previous space deployment. Results of system requirements analysis favour the deployment of large area detectors. Analysis of the in-flight impact sensor signals yields the position, time and exposure pointing direction of the tracks containing the impactor residues, which are analysed after retrieval. (C) 1999 COSPAR. Published by Elsevier Science Ltd.
  • SHIBATA Hiromi, KOBAYASHI Koichi, IWAI Takeo, HAMABE Yoshimi, SASAKI Sho, HASEGAWA Sunao, YANO Hajime, FUJIWARA Akira, OHASHI Hideo, KAWAMURA Toru, NOGAMI Ken'ichi
    25 107-110, Nov 20, 1999  Peer-reviewed
  • YANO Hajime, FUJII Yasumasa
    Planetary People, 8(1) 4-16, Mar 25, 1999  Peer-reviewedLead authorCorresponding author
  • T. Nakamura, H. Yano
    Antarctic Meteorite Research, 12, 183-198 183-198, 1999  Peer-reviewed
  • M Yamada, S Sasaki, H Nagahara, A Fujiwara, S Hasegawa, H Yano, T Hiroi, H Ohashi, H Otake
    EARTH PLANETS AND SPACE, 51(11) 1255-1265, 1999  Peer-reviewed
    For the purpose of simulating the surface alteration process called "space weathering", experiments of pulse laser irradiation, proton implantation, and laser irradiation to proton implanted samples were performed and reflectance spectra of altered materials were measured. To simulate the impact heating by micrometeorite bombardments, we made a new apparatus using a pulse laser whose pulse duration is 6-8 nanoseconds, comparable with a timescale of micrometeorite impacts. We find that the degree of space weathering, i.e., change of reflectance spectrum should depend on mineral composition. Laser irradiation onto olivine produces the largest reduction of albedo and the highest reddening of reflectance spectrum. In general, variation of olivine spectra is much larger than that of pyroxenes, Depths of absorption bands do not change in the scaled spectra, The olivine spectrum after the laser irradiation can match spectra of some olivine asteroids within a subtype of S-type asteroids. Comparison of Vesta spectrum with altered pyroxene spectra suggests that Vesta surface would be relatively older than olivine asteroids. We also investigate the influence of solar wind proton and pyroxene FeO content. The proton implantation causes small changes in olivine and enstatite spectra. Implanted protons do not influence spectral change by the laser irradiation: the laser irradiation and the proton implantation do not produce multiplicative but additive changes on the reflectance spectra, FeO content of pyroxenes does not relate to the degree of reflectance change.
  • H Yano
    EARTH PLANETS AND SPACE, 51(11) 1233-1246, 1999  Peer-reviewedLead authorCorresponding author
    This paper reviews major results of present studies and recent developments for future missions in the Japanese space program regarding in-situ measurement and collection of micrometeoroids and orbital debris in the near Earth space. Japan's contribution in this area began with the post flight impact analysis of the Space Flyer Unit (SFU) satellite which was returned to Earth in 1996 after 10-month exposure in space. Despite a decade later than similar efforts first conducted in the USA and Europe, it resulted in a record of over 700 hypervelocity impact signatures, which now forms the nation's first database of real space impacts being open to public in the Internet. Together with laboratory impact tests, both morphological and elemental analyses of the impact craters yielded new insights of the meteoroid to debris ratio as well as flux variation compared with the previous spacecraft. The next step was a passive aerogel exposure in the STS-85 shuttle mission in 1997. No hypervelocity impact was found there but its experience has been incorporated for designing a microparticle collector to be on-board the Japan Experiment Module-Exposed Facility of the International Space Station. All of such "passive" collection of micro-impact features, however, still leave the significant uncertainty in the quest of their origins. Therefore an aerogel-based "hybrid" dust collector and detector (HD-CAD) is currently under the development. It measures time of impact and deduces impactors' orbital and physical parameters by detecting impact flash while still capturing them intact. The system is suitable for both (1) sample return missions in LEO as well as to parent bodies of meteoroids, i.e., comets and asteroids, and (2) one-way mission to where the thermal and plasma environment is such that impact induced plasma detectors may suffer from significant noise, e.g., a Mercury orbiter and a solar probe. Together with unambiguous dust samples from a comet by STARDUST and an asteroid by MUSES-C as references, the HD-CAD in the LEO will be able to deduce the accretion rates of the cometary and asteroidal dust grains on the Earth.
  • S Hasegawa, A Fujiwara, H Yano, T Nisimura, S Sasaki, H Ohashi, T Iwai, K Kobayashi, H Shibata
    Advances in Space Research, 23(1) 119-122, 1999  Peer-reviewed
    Micrometeoroid detection in space usually involves high-velocity impact phenomena. In-situ dust detectors should be calibrated by a microparticle accelerator with a mass and velocity range comparable to micrometeoroids. A pilot model of an accelerator was constructed some years ago and fundamental research for an advanced facility has been performed. We are developing two new accelerators. A 3.75MV Van de Graaff electrostatic accelerator at The Research Center for Nuclear Science and Technology, University of Tokyo, has been modified to accelerate microparticles, and acceleration testing is now being carried but. The expected velocity range is 1-20 km/s for micron or sub-micron particles. Another small accelerator will be installed for easier handling, more frequent use, and lower-cost operation. (C) 1999 COSPAR. Published by Elsevier Science Ltd.
  • H Akiyama, A Shiraishi, J Haruyama, J Terazono, H Yano
    Advances in Space Research, 23(2) 367-370, 1999  Peer-reviewedLast author
    Recent close encounters to Europa, a giant Jovian satellite, by the Galileo spacecraft reenforced the hypothesis that there might exist a liquid ocean of H2O in Europa. It can be assumed that Europa, like the Earth, has biological systems under its sub surface ocean, and that marine organisms consume chemical nutrients released by geological activities even though there is no sunlight. The purpose of this paper is to introduce conceptual and feasibility studies of a spacecraft mission to explore Europa's hypothetical sub-surface ocean. In this paper, we present possible searches for the possible biological evidence through the observation of traces. We analyze the scientific rationale, the methodology and the instrumentation of our investigation held in this mission. The designs of spacecraft and mission profile is' also reviewed. (C) 1999 COSPAR. Published by Elsevier Science Ltd.
  • MJ Neish, S Kibe, H Yano, SP Deshpande, K Morishige
    Advances in Space Research, 23(1) 101-111, 1999  Peer-reviewed
    The Space Flyer Unit (SFU) has provided investigators in Japan with our first opportunity to conduct an extensive post-flight analysis (PFA) of particulate impacts on a retrieved satellite, and thereby further our goals in space debris research (Kibe et al., 1997). The PFA has now been in progress for some time, and in this paper the present status of our investigations is reported, our findings to date are briefly summarised, and finally a plan for the immediate future is outlined. (C) 1999 COSPAR. Published by Elsevier Science Ltd.
  • K Morishige, H Yano, Y Maekawa, SP Deshpande, MJ Neish, S Kibe
    Advances in Space Research, 23(1) 113-117, 1999  Peer-reviewedCorresponding author
    We report on three dimensional morphology of about 100 hypervelocity impact craters on the Teflon radiators of the SFU spacecraft measured by scanning laser microscope and X-ray CT technique. We also performed impact calibration experiments using a two-stage light-gas gun at ISAS with alumina, glass and copper bead projectiles of diameters 50 to 80 mu m at velocities from 3.5 to 4.5 km/s, in order to reproduce impact crater profiles formed in space. As a result, the depth to diameter ratio of these impact craters constrains bulk density, velocity and size of impactors, which are complementary information to elemental analysis regarding the origin of the impactors, namely meteoroids or space debris. (C) 1999 COSPAR. Published by Elsevier Science Ltd.
  • M Ishiguro, R Nakamura, Y Fujii, K Morishige, H Yano, H Yasuda, S Yokogawa, T Mukai
    ASTROPHYSICAL JOURNAL, 511(1) 432-435, Jan, 1999  Peer-reviewed
    We present the first ground-based observational evidence of the zodiacal dust bands originally discovered by the Infrared Astronomical Satellite (IRAS) and confirmed by the Cosmic Background Explorer (COBE). Our photometric observations have been performed on Mauna Kea, Hawaii, between 1997 October 29 and November 2, using a 24 mm wide-angle lens attached to a cooled CCD camera, and a blue filter centered at 440 nm. Photometric data of the morning zodiacal light have revealed the presence of zodiacal dust bands at ecliptic latitudes beta = 0 degrees, 3 degrees, and +/- 10 degrees, as well as additional faint structures at approximately beta = +/- 5 degrees, between solar elongations epsilon = 75 degrees and 90 degrees. The brightness of dust bands is approximately 2%-3% of the background zodiacal light. Moreover, our observation of the Gegenschein has discovered dust bands at beta = +2 degrees, -4 degrees, and -9 degrees at 165 degrees less than or equal to epsilon less than or equal to 185 degrees. Using the separation of the inner dust band pair observed in two different regions of epsilon, we estimate the parallactic distance of this band pair to be about 1.6 AU from the Sun.
  • M. J. Burchell, R. Thomson, H. Yano
    Planetary and Space Science, 47(1-2) 189-204, Dec 15, 1998  Peer-reviewedLast author
    We have investigated in the laboratory the capture in aerogel (density 92.5±0.5 kg m-3) of small particles travelling at (5.1±0.2) km s-1. The particles used were soda glass spheres and irregularly shaped olivine and iron particles, with mean diameters in the range 75-355 microns. We have measured the impact site for each particle, characterised by the mean diameter of the entrance hole in the aerogel, the minimum and maximum radii of the damaged region in the surface of the aerogel around the entrance hole, the length of the track in the aerogel caused by passage of the particle into the aerogel's interior, and the diameter of the captured particle (if seen) found near the end of the track. For each type of particle we establish relationships between the observed parameters and the pre-impact particle size. We find that the processes resulting in the observed surface features and the capture of the particles in the interior of the aerogel are different. We also find that the particle shape (spherical/irregular) does not unduly influence penetration depths in the aerogel. We have studied the effects of non-normal incidence on the observed impact features and find that the angle of incidence can be reconstructed to within ±2°. We compare the laboratory obtained data with that measured for four particles captured in a sample of aerogel flown in a Low Earth Orbit on board the EuReCa spacecraft. The density of one of the particles is predicted to be (1776±346) km m-3. Using the ability to reconstruct impact direction the probable nature of the particles is shown to be micrometeoroids with retrograde trajectory. © 1999 Elsevier Science Ltd. All rights reserved.
  • Yano Hajime, Noguchi Takaaki
    Antarctic Meteorite Research, 11 136-154, Mar, 1998  Peer-reviewedLead authorCorresponding author
    Based on our initial visual selection (IVS) criteria and low vacuum (LV)-SEM/EDS data, we successfully selected candidates of unmelted chondritic Antarctic micrometeorites (AMMs) from the unsorted sample set collected by Maurette's group in 1991. AEM data of some of the selected microparticles show that they are unmelted but probably dehydrated AMMs. An AMM candidate, 91-1-C4,contains ferroan (around Fo30) olivine grains which have planar channels parallel to (001). Their textures quite resemble those shown in the initial stage of iddingsite formation of olivine phenocrysts in terrestrial b...
  • 矢野創, 中村智樹, 野崎航, 船木実, 今栄直也, 野上謙一
    地球化学, 32(4) 161-174, 1998  Peer-reviewedLead authorCorresponding author
    Since the early development of the cosmic dust research that started almost a century ago, a wide variety of the sample collection techniques has been developed. Such direct sampling of cosmic dust (or micrometeoroids, micrometeorites, interplanetary dust particles (IDP)) has enabled subsequent analyses of these extra-terrestrial micro particles at ground laboratories in great detail. In coming years, Japan will have an array of new opportunities of cosmic dust collection from space, stratosphere and Antarctica. However each collection site causes certain biases of samples in terms of physical and chemical alterations, selection effects and contamination. Here we review the cosmic dust collection from deep sea sediments, Greenland blue lakes, Antarctic ice cores, stratosphere and both near-Earth and interplanetary space, together with a brief description of the curation system of the samples being operated by NASA/JSC.
  • Hajime Yano
    Preserving the Astronomical Windows, 1998  
  • S Abe, H Yano, N Ebizuka, J Watanabe
    EARTH MOON AND PLANETS, 82-3 369-377, 1998  Peer-reviewed
    During the 1999 Leonids, an intensified HDTV camera was used for slitless meteor spectroscopy at visible and near-UV wavelengths in three night flights of the Leonid Multi-instrument Aircraft Campaign. The IIDTV system provided a high dynamic range (digital 10-bit) and a wide field of view of 37 x 21 degrees. The maximum spectral sensitivity is at 405 nm, while the resolving power of the spectrograph was lambda/Delta lambda similar to 250. Here, we report on the results for one particularly nice spectrum from a Leonid meteor at 03:24:40 UT. Numerous atomic emission lines of magnesium and iron were detected, with an excitation temperature of T = 5,000 +/- 1,000. It is confirmed that sodium is released from the meteoroid earlier than iron and magnesium, just as in meteors of the 1998 Leonid shower. Rovibrational bands of N-2 dominate the spectrum in the visible and near-IR. We searched for CN band emission at 389 nm, but could not detect it due to the overlap of numerous iron lines.
  • YANO Hajime
    Planetary people, 6(4) 281-283, Dec 1, 1997  
  • Sunil Deshpande, Michael Neish, Hajime Yano, Seishiro Kibe
    Advances in the Astronautical Sciences, 96 1021-1031, Dec 1, 1997  Peer-reviewed
    In January 1996, STS-72 (OV-105) successfully retrieved the Space Flyer Unit (SFU). Japan's first retrievable spacecraft had successfully completed it's 10 month mission in LEO at an orbital altitude of some 480km and inclination of 28.5̊. Once returned to Kennedy Space Centre and removed from the pay load bay a post flight investigation of SFU commenced. This investigation continued whilst SFU underwent safing procedures in the Astrotech Facility (ASO), Florida, and on it's return to Japan. Since de-integration of the payloads, from SFU, all exposed surfaces have been designated for detailed scanning and configuration control to determine the impact damage received from micrometeoroid and space debris particulates. In accordance with IADC and in light of the advent of the International Space Station all the data collected from this investigation shall be made available to the public and archived. To this end the SFU archive is being created as part of NAL's World Wide Web site (WWW). The WWW pages hold all images related to impact sites located on the SFU surfaces including multi-layer insulation MLI (aluminised Kapton™ top surface) second surface mirrors SSM (silvered Teflon™ top surface), scuff plates (painted aluminium). These images were taken at various magnifications (100-800x) and focal depths to determine and measure features seen. The results of the primary analysis (measured hole diameters etc.) are also available on the WWW site. This paper describes the current contents of the WWW site, showing examples of the pages and images available, plans for further development and updating and access information.
  • M. J. Neish, S. P. Deshpande, S. Kibe, H. Yano, Y. Kitazawa, S. Yamamoto
    European Space Agency, (Special Publication) ESA SP, (393) 177-182, Dec 1, 1997  Peer-reviewed
    The Space Flyer Unit (SFU) was retrieved by the space shuttle in January 1995, and is presently being subjected to a post-flight analysis with emphasis on the detection and documentation of hypervelocity impact features from space debris and micrometeoroids. A summary of the analysis procedure is presented here. Some results from preliminary eye surveys are also provided. In addition, more detailed results from high-resolution imaging of craters on two peripheral second-surface mirrors (SSMs) are given, and the morphology of the craters detected in these surfaces is discussed. First results of hypervelocity impact calibration tests are also included.
  • T Yada, H Yano, T Nakamura, N Takaoka
    METEORITICS & PLANETARY SCIENCE, 32(4) A144-A144, Jul, 1997  
  • Sunil P. Deshpande, Carl R. Maag, Seishiro Kibe, Michael Neish, Hajime Yano
    Space Technology, 17(2) 103-112, Mar 1, 1997  Peer-reviewedLast author
    In January 1996, STS-72 successfully retrieved Japan's Space Flyer Unit after a 10-month excursion in low Earth orbit. It was apparent from observations of the spacecraft that many surfaces had undergone changes from pre-flight condition. Not unlike other retrieved spacecraft (EuReCa, LDEF), SFU exhibited signs of impact damage, atomic oxygen erosion effects and general "wear and tear". During ground operations at Astrotech, Florida, the opportunity was afforded to inspect SFU for the effects of contamination and document impact sites and other interesting features. In total 16 wipes were taken from around the periphery of the spacecraft, along MLI interfaces and special areas of interest. All faces were wiped to determine any directionality dependence with regard to material deposition. Alongside the wiping of the spacecraft a set contamination monitors and witness plates were installed around the SFU and MGSE to observe the molecular deposition/non-volatile residue (NVR) and particle fallout that occurred during the de-servicing period in the ASO HPF (post hydrazine de-servicing) and a second set deployed to monitor fallout during the shipment back to Japan. The results of the contamination wipes and monitors are presented here. © 1998 Elsevier Science Ltd.
  • H Yano, S Kibe, SP Deshpande, MJ Neish
    Advances in Space Research, 20(8) 1489-1494, 1997  Peer-reviewedLead authorCorresponding author
    The Space Flyer Unit (SFU) was retrieved from space after its 10-month mission in January 1996. Here we report the first findings from the post flight analysis of its Kapton MLI and Teflon radiators in terms of impact flux, crater morphology and implications of impactors' origins. The impact flux on the Sun face is also compared with the LDEF, EuReCa and HST data. On the Kapton MLI, some directional information can be deduced and its capture cell Structure promises a high survivability of, residues for chemical analysis. The peripheral flux variation is not inconsistent with the EuReCa data favouring for the Earth's apex. The anti-sun face flux exceeded the Sun face by a factor of 1.7. The size distribution index of the impact features on the Sun face Teflon agreed with the certain size ranges of the previous spacecraft. Plans of forthcoming studies such as detailed CCD/laser scanning, calibration impact experiments and chemical analysis are also addressed. (C) 1997 COSPAR. Published by Elsevier Science Ltd.
  • 日本惑星科学会誌「遊・星・人」, 6, No.4. 281-350, 1997  Peer-reviewedLead authorCorresponding author
  • 大橋英雄, 北沢幸人, 矢野創
    日本惑星科学会誌 遊・星・人, 6(4) 312-325, 1997  Peer-reviewedLast author
  • S Deshpande, M Neish, H Yano, S Kibe
    SPACE COOPERATION INTO THE 21ST CENTURY, 96 1021-1031, 1997  Peer-reviewed
    In January 1996, STS-72 (OV-105) successfully retrieved the Space Flyer Unit (SFU). Japan's first retrievable spacecraft had successfully completed it's 10 month mission in LEO at an orbital altitude of some 480km and inclination of 28.5 degrees. Once returned to Kennedy Space Centre and removed from the payload bay a post flight investigation of SFU commenced This investigation continued whilst SFU underwent safing procedures in the Astrotech Facility (ASO), Florida, and on it's return to Japan. Since de-integration of the payloads, from SFU, all exposed surfaces have been designated for detailed scanning and configuration control to determine the impact damage received from micrometeoroid and space debris particulates. In accordance with IADC and in light of the advent of the International Space Station all the data collected from this investigation shall be made available to the public and archived. To this end the SFU archive is being created as part of NAL's World Wide Web site (WWW). The WWW pages hold all images related to impact sites located on the SFU surfaces including multi-layer insulation MLI (aluminised Kapton(TM) top surface) second surface mirrors SSM (silvered Teflon(TM) top surface), scuff plates (painted aluminium). These images were taken at various magnifications (100-800x) and focal depths to determine and measure features seen. The results of the primary analysis (measured hole diameters etc.) are also available on the WWW site, This paper describes the current contents of the WWW site, showing examples of the pages and images available, plans for further development and updating and access information.
  • MJ Neish, H Yano, S Kibe, SP Deshpande, Y Kitazawa, S Yamamoto
    7TH INTERNATIONAL SYMPOSIUM ON MATERIALS IN SPACE ENVIRONMENT, 399(399) 477-484, 1997  Peer-reviewed
    Presented here are the latest results of the post-flight analysis of the Space Flyer Unit, Japan's first retrievable spacecraft. The morphology of impact features in silverised Teflon second-surface mirrors (SSMs) and Kapton multi-layer insulation (MLI) is Morphological comparisons are made between laboratory and space impacts into MLI material. Flux figures are shown for various SFU surfaces and compared with fluxes from earlier spacecraft, such as the Long Duration Exposure Facility and EuReCa. A summary of the hypervelocity impact calibration programme is given, including laboratory tests carried out at 5 km s(-1) and around 3.5 km s(-1) into Kapton film of various thicknesses. The results of these tests are shown.
  • YANO Hajime
    Planetary people, 5(4) 209-218, Dec 1, 1996  Peer-reviewedLead authorCorresponding author
  • H Yano
    OBSERVATORY, 116(1133) 256-257, Aug, 1996  Peer-reviewedLead authorCorresponding author
  • H. Yano
    Advances in Space Research, 17(12) 189-192, 1996  Peer-reviewedLead authorCorresponding author
    Extensive studies of over 100 impact sites on aluminium foils and mesh supports of the Timeband Capture Cell Experiment (TiCCE) on the European Retrievable Carrier (EuReCa) spacecraft were conducted with scanning electron microscope and energy dispersive X-ray spectrum analyser. Chemical elements of residues in and around the perforations and craters were examined to identify the origin of impactors. 73 % of the impacts were classified; the minimum of 15 % was due to natural particle impacts and the rest indicated high silicon presence. Possible origins of these silicon profiles were discussed. For micrometeoroid craters, the depths to diameter ratios were compared with those of meteoroid and orbital debris impacts on the Solar Maximum Mission satellite.
  • NRG Shrine, EA Taylor, H Yano, AD Griffiths, JAM McDonnell
    CHARACTERISTICS AND CONSEQUENCES OF ORBITAL DEBRIS AND NATURAL SPACE IMPACTORS, 2813 76-87, 1996  Peer-reviewed
    On retrieval from Low Earth Orbit (LEG), the solar arrays from the European Retrievable Carrier(EuReCa) and one solar array wing of the Hubble Space Telescope (HST) were inspected for micrometeoroid and space debris impact damage. 703 and 814 impact sites respectively were analysed in detail. Interpretation of particle parameters from this large data set can yield a useful measurement of the micrometeoroid and debris flux in LEG. Due to similar orbital parameters, this then provides a flux measurement complimentary to those measured by the Timeband Capture Cell Experiment (TiCCE) of the EuReCa spacecraft and detectors and exposed surfaces on the Long Duration Exposure Facility (LDEF). To allow comparison of data from the space retrieved solar cells to previous data, solar cell material, glass and aluminium targets were impacted for inter-calibration using the University of Kent's Light Gas Gun (LGG). An average of 20 impact sites on each target material per shot were measured. It was decided to consider only non-perforations of the 150 micron thick CMX cover glass, common to both EuReCa and HST solar cells. Trends in crater morphology of the laboratory impacts are discussed and compared to those from space impacts. The effects of impact angle and crater scaling with particle size are investigated and a conversion from appropriate solar cell crater parameters to the ballistic limit in aluminium is presented.
  • WG TANNER, JAM MCDONNELL, H YANO, HJ FITZGERALD, DJ GARDNER
    Advances in Space Research, 17(12) 201-204, 1995  Peer-reviewed
    The continued analyses of penetrating impacts on MAP foils of Aluminium and Brass have produced data for several LDEF faces, i.e., Space, West, and East. These data have immediate bearing on the interpretation and design of devices to detect the penetration of a thin metallic firm by a dust grain which have been tested both in the laboratory and in space. A crucial component of the analysis has been the theoretical calculation utilizing CTH, a Sandia National Laboratory Hydrodynamic computer code/1/ to assess the parameters of the hypervelocity penetration event. In particular theoretical hydrodynamic calculations have been conducted to simulate the hypervelocity impact event where various cosmic dust grain candidates, e.g., density = 0.998, 2.700, 7.870 (gm/cm(3)), and velocities, i.e., 7 - 16 km/s, have been utilized to reproduce the events. Theoretical analyses of hypervelocity impact events will be reported which span an extensive matrix of values for velocity, density and size. Through a comparison between LDEF MAP foil measurements and CTH hydrocode calculations these analyses will provide an interpretation of the most critical parameters measured for space returned materials, i.e., for thin films, the diameter of the penetration hole, D-h, and for semi-infinite targets, the depth-to-diameter ratio of craters, D-c/T-c. An immediate consequence of a comparison, of CTH calculations with space exposed materials will be an enhancement of the coherent model developed by UKC-USS researchers to describe penetration dynamics associated with LDEF MAP foils.
  • YANO Hajime
    Planetary People, 3(1) 30-41, Mar 25, 1994  Peer-reviewedLead authorCorresponding author
  • H YANO, JAM MCDONNELL
    SEVENTY-FIVE YEARS OF HIRAYAMA ASTEROID FAMILIES: THE ROLE OF COLLISIONS IN THE SOLAR SYSTEM HISTORY, 63 161-167, 1994  Peer-reviewed
  • YANO H, FITZGERALD H J, TANNER W G
    Planetary and Space Science, 42(9) 793-802, Jan 1, 1994  Peer-reviewedLead authorCorresponding author
    In situ collection of cosmic dust and space debris on the Low Earth Orbit has yielded a new perspective of the near Earth dust environment. The hypervelocity impact craters on the trailing side of the Long Duration Exposure Facility were converted into the projectile sizes and the physical and elemental comparison with interplanetary dust particles captured in the stratosphere was carried out. The size distribution agreed well while some chemical elements of LDEF samples suggested a fluctuation due to massive energy transfer during the hypervelocity impact in space. A possible selection process is discussed. Also, future opportunity of in situ detection of meteor showers is foreseen as long as new intact-capture materials are properly developed. © 1994.
  • YANO Hajime
    Planetary People, 2(4) 193-205, Dec 1, 1993  Peer-reviewedLead authorCorresponding author
  • YANO Hajime
    Planetary People, 2(3) 133-143, Sep 25, 1993  Peer-reviewedLead authorCorresponding author
  • H YANO, PJ NEWMAN, JAM MCDONNELL
    Advances in Space Research, 13(8) 111-114, 1993  Peer-reviewedLead authorCorresponding author
    One section of the double layer capture cell of the space pointing face on the LDEF was studied with SEM/EDX. Analysis of chemical composition of residues and and ellipticity of craters on the second layer enabled them to match up with top layer penetrations which caused the secondary cratering. Morphological feature of the second layer was described. A possible direction of an impact was suggested whilst some Si particles and a mafic fragment were detected as evidences of micrometeoroid impacts. Origins of contaminations were also discussed. © 1993.
  • HIGASHI Akira, SASAKI Kenji, YANO Hajime, OHARA Manami
    Proceedings of the NIPR Symposium on Polar Meteorology and Glaciology, 6 155-155, Dec, 1992  Peer-reviewed
    SEM observations have been carried out since 1987 with microparticales contained in medium and shallow depth ice cores retrieved at Mizuho Station (1984 : 70°42'S, 44°20'E, 2230m) and at the Advance Camp (1985,74°12'S, 34°59'E, 3200m) in East Queen Maud Land, Antarctica. Results of observations including morphological classification of particles have been published (HIGASHI et al. : Bull. Galcier Res., 8,31,1990). Addition of observational data from cores of shallow depth at Mizuho, and Asuka Stations (1989 : 71°34'S, 24°08'E, 930m) in Antarctica, and also at Site J in Greenland (1989 : 66°...

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