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    宇

    宇宙航空研究開発機構

    Japan Aerospace Exploration Agency
    EST. 2003
    5,071论文总数
    10.1万引用总数

    The Japan Aerospace Exploration Agency (JAXA) (国立研究開発法人宇宙航空研究開発機構, Kokuritsu-kenkyū-kaihatsu-hōjin Uchū Kōkū Kenkyū Kaihatsu Kikō, literally "National Research and Development Agency on Aerospace Research and Development") is the Japanese national air and space agency. Through the merger of three previously independent organizations, JAXA was formed on 1 October 2003. JAXA is responsible for research, technology development and launch of satellites into orbit, and is involved in many more advanced missions such as asteroid exploration and possible human exploration of the Moon. Its motto is One JAXA and its corporate slogan is Explore to Realize (formerly Reaching for the skies, exploring space).

    论文量&引用量时间轴

    机构学者

    排序
    T. Mukai
    T. Mukai
    Japan Aerospace Exploration Agency, The Institute of Space and Astronautical Science
    论文:133引用:0H-index:0
    Fujii Kozo
    Fujii Kozo
    Faculty of Engineering, Department of Information and Computer Technology, Tokyo University of Science
    论文:93引用:0H-index:0
    Kazuo Makishima
    Kazuo Makishima
    Kavli Institute for the Physics and Mathematics of the Universe, University of Tokyo;Graduate School of Science, University of Tokyo;Cosmic Radiation Laboratory, Institute of Physical and Chemical Research
    论文:68引用:0H-index:0
    Tatsuaki Okada
    Tatsuaki Okada
    ISAS/JAXA
    论文:66引用:0H-index:0
    Yuichi Tsuda
    Yuichi Tsuda
    Japan Aerospace Exploration Agency
    论文:55引用:0H-index:0
    Ayako Matsuoka
    Ayako Matsuoka
    Institute of Space and Astronautical Science
    论文:53引用:0H-index:0
    Hideo Matsuhara
    Hideo Matsuhara
    Japan Aerospace Exploration Agency
    论文:51引用:0H-index:0
    Kazuhiro Nakazawa
    Kazuhiro Nakazawa
    Division of Experimental Studies, Nagoya University;Kobayashi-Maskawa Institute for the Origin of Particles and the Universe, Nagoya University;Graduate School of Science, Nagoya University
    论文:44引用:0H-index:0
    Kazuomi Yamamoto
    Kazuomi Yamamoto
    Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency
    论文:41引用:0H-index:0

    论文(5072)

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    1Ryugu Reference Project: Recommendations from the Measurement Definition Team
    Tetsuya Yokoyama, Guillaume Avice, Henner Busemann, Nicolas Dauphas, Daniel P. Glavin, Ashley J. King, Thorsten Kleine, Katharina Lodders, Frederic Moynier,Maria Schonbachler, Yoshinori Takano, Kun Wang,

    Sample return missions play a significant role in planetary science by providing pristine extraterrestrial materials. JAXA's Hayabusa2 and NASA's OSIRIS-REx missions have returned samples from the C-type asteroids Ryugu and Bennu, respectively. The chemical and mineralogical compositions of these samples closely resemble those of CI chondrites, the traditional reference material for solar system abundances. Based on the findings of the Hayabusa2 mission, JAXA launched the Ryugu Reference Project (RRP) to maximize the scientific value of the returned samples and formed the RRP Measurement Definition Team (RRP-MDT) to elucidate the RRP's scientific goal and objectives. The RRP-MDT defined the goal of RRP to reassess the elemental abundances and isotopic compositions of the solar system through comprehensive analyses of the returned asteroid samples and CI chondrites. To this end, the team recommended preparing homogeneously powdered Ryugu reference materials (RRM) using approximately 750 and 400 mg of samples from Chambers A and C, respectively, to address observed compositional heterogeneities. The team proposed to measure the elemental abundances and isotopic compositions of the RRM by analytical techniques involving seven specific measurement groups. Through comprehensive analytical methodologies, interlaboratory calibration, and statistical evaluation, the RRP aims to refine our understanding of solar system formation and evolution.

    2026METEORITICS & PLANETARY SCIENCE(2026)引用:98
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    2Fused Multi-Filament Fabrication of Continuous Carbon Fiber-Reinforced Polymer Composites
    Kousei Obata, Naruki Ichihara,Masahito Ueda, Keisuke Iizuka

    A fused multi-filament fabrication (FmFF) method for the 3D printing of continuous carbon fiber-reinforced polymer (cCFRP) composites was proposed as an extension of the fused filament fabrication (FFF) method. The FmFF method enables the simultaneous deposition of multiple filaments using a single nozzle. The effect of simultaneous multi-filament deposition on the quality and mechanical properties of 3D-printed cCFRP composites was evaluated. Specifically, the FmFF process was investigated using a simultaneous five-filament deposition process, with the five filaments being integrated into a bundle and printed using a single nozzle. The quality differed depending on the path. In straight sections, the filament bundles were arranged in a regular pattern, whereas in curved sections, they were arranged unevenly owing to filament movement. The tensile and bending moduli of the cCFRP composites fabricated using the FmFF method (59 GPa and 50 GPa using Vf = 0.3 filaments) were almost identical to those obtained using the FFF method (60 GPa and 51 GPa). However, the bending strength was relatively low (FmFF: 451 MPa, FFF: 540 MPa), whereas the tensile strength was higher due to a larger curvature radius in the FmFF nozzle (FmFF: 1090 MPa, FFF: 800 MPa). Moreover, the bending failure mode was partial fragmentation and delamination, indicating relatively low interfacial adhesion between the layers. This study demonstrates the applicability of the FmFF method for high-throughput fabrication of lightweight small structural parts, while simultaneously identifying future challenges for improvement.

    2026Progress in Additive Manufacturing(2026)引用:24
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    3In-Situ Photoelastic Imaging Method for Quantifying Stress Waves in Glass Subjected to Hypervelocity Impact of Debris
    M. Nagano, N. Kawai, S. Hasegawa, S. Yoshida, E. Sato

    Hypervelocity impacts of small objects, such as space debris, pose significant challenges to the structural reliability of glass due to the extreme stresses and crack propagation they induce. While conventional optical techniques can qualitatively observe stress wave propagation, quantitative evaluation of stress fields and their association with fracture mechanisms remains a critical gap. This study aims to develop and validate a novel in situ photoelastic imaging method for quantitatively analyzing stress wave propagation behavior in glass under hypervelocity impact conditions. A new combined experimental and analytical system was developed using a two-stage light-gas gun to conduct hypervelocity impact experiments on silica glass plates (dimensions: 60 × 60 × 15 mm3). Both linear- and circular-polarized photoelastic images were obtained during the experiments using synchronized high-speed cameras. Time-dependent stress fields were calculated via an integrated photoelasticity approach using the onion-peeling method, which was reformulated into an integral representation to accommodate general axisymmetric conditions. The proposed analysis method successfully determined time-dependent stress-fields in impacted glass plates. Longitudinal stress waves exhibited wavelength elongation due to mechanical responses near the elastic limit under hypervelocity conditions. Observations also revealed dynamic interactions between stress wave propagation and crack initiation, highlighting the critical role of back-surface-reflected stress waves in fracture initiation. This study demonstrates the utility of in situ photoelastic observation combined with quantitative analysis for exploring stress wave behavior and subsequent fracture mechanisms in glass. The proposed method has the potential to advance the understanding of dynamic material behavior and improve the design and reliability of glasses in high-energy applications, such as space debris protection.

    2026Experimental Mechanics(2026)引用:13
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    4Variational Mode Decomposition Analysis of the Relationship Between Low-Frequency Shock-Wave Oscillations and Buffet Cells
    Yuya Ohmichi, Yosuke Sugioka

    This study investigates the relationship between low-frequency shock-wave oscillations and buffet cells on the main wing of the NASA common research model. The flow conditions were set at a Mach number of 0.85, Reynolds number of 2.27 x 106, and angle of attack of 4.82 degrees. Buffet cells are cellular patterns with spanwise periodicity that propagate toward the wing tip, with nondimensional frequencies (Strouhal numbers) of 0.2-0.6, higher than those of shock oscillations associated with transonic buffet. However, the physical mechanisms driving buffet cells and their interaction with low-frequency shock motion are not fully understood. This study employs variational mode decomposition-based nonstationary coherent structure (VMD-NCS) analysis applied to unsteady pressure-sensitive paint measurement data. The results reveal that the amplitude of buffet cells is not directly coupled to the low-frequency shock-wave oscillations but instead shows correlation with the boundary layer separation state. Strong buffet cell fluctuations persist in regions of sustained separation (midspan), while their amplitude varies with local separation/reattachment dynamics in regions of intermittent separation (outboard). These observations suggest that shock-waves are important to generate the adverse pressure gradient necessary for boundary layer separation, but their influence on buffet cells depends on the resulting separation behavior. This insight from experimental observations in this study is consistent with previous computational studies suggesting that buffet cell behavior depends on boundary layer separation characteristics. Moreover, this study demonstrates the effectiveness of VMD-NCS analysis for investigating nonstationary fluid phenomena with multiple spatial and temporal patterns.

    2026AEROSPACE SCIENCE AND TECHNOLOGY(2026)引用:2
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    5JWST Reveals Extended Stellar Disks for ALMA-bright Dusty Star-Forming Galaxies in the Spiderweb Protocluster
    Y. H. Zhang, H. Dannerbauer, J. M. Perez-Martinez, Y. Koyama, X. Z. Zheng, R. Calvi, Z. Chen, K. Daikuhara,C. De Breuck, C. D'eugenio, B. H. C. Emonts, S. Jin,

    We present JWST/NIRCam imaging of dusty star-forming galaxies (DSFGs) detected by the Atacama Large Millimetre/submillimetre Array (ALMA) in the Spiderweb protocluster at z = 2.16. We identified 22 DSFGs detected by both ALMA and JWST, ten of which are spectroscopically confirmed as protocluster members. This is the first systematic analysis of a statistical DSFG sample in z ∼ 2 protocluster environments using JWST/NIRCam data. Most of the DSFG members exhibit red colours and reside in the dusty star-forming region of the rest-frame UVJ diagram, indicating strong dust obscuration. The Gini-M20 diagram suggests that most DSFGs in this protocluster are late-type disks, with a significant fraction displaying clumpy and disturbed rest-frame UV/optical morphologies, but few showing clear merger signatures. The DSFG members exhibit relatively large stellar disks and effective radii with a median stellar mass of log(M/M⊙) = 10.8 ± 0.3, placing them above coeval field DSFGs and typical protocluster galaxies in the size–mass relation at both rest-frame optical and near-infrared wavelengths. These sizes are comparable to those of more evolved field DSFGs at z ∼ 1 − 2, indicating accelerated structural growth in dense environments. Moreover, these DSFG members show a decreasing trend in stellar size from shorter to longer wavelengths, with a moderately steep slope comparable to coeval field DSFGs. These results may support an inside-out growth scenario for protocluster evolution, in which massive galaxies near the centre are more evolved and more strongly affected by active galactic nucleus feedback and environmental effects, for example, ram-pressure stripping. We propose that the cold gas accretion at the protocluster outskirts drives intense star formation and stellar disk growth in ALMA-detected DSFGs, which are expected to evolve into massive elliptical galaxies at later stages.

    2026ASTRONOMY & ASTROPHYSICS(2026)引用:2
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    合作机构(100)

    东京大学合作论文 1,019
    名古屋大学合作论文 529
    京都大学合作论文 383
    东北大学(日本)合作论文 342
    戈达德太空飞行中心合作论文 249
    大阪大学合作论文 227
    东京工业大学合作论文 217
    日本国立天文台合作论文 172
    东京都立大学合作论文 168
    广岛大学合作论文 159

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