研究者業績

白石 浩章

シライシ ヒロアキ  (Hiroaki Shiraishi)

基本情報

所属
国立研究開発法人宇宙航空研究開発機構 宇宙科学研究所太陽系科学研究系 助教
総合研究大学院大学 物理科学研究科 宇宙科学専攻 助教

J-GLOBAL ID
200901067190591293
researchmap会員ID
5000019313

論文

 6
  • 白石 浩章, 白井 慶, 石原 吉明, 早川 雅彦, 水野 貴秀, 後藤 健, 尾崎 正伸, 山田 和彦, 田中 智, 山田 竜平, 及川 純, 村上 英記
    日本火山学会講演予稿集 2016 66-66 2016年  
  • Ryuhei Yamada, Tanguy Nebut, Hiroaki Shiraishi, Philippe Lognonne, Naoki Kobayashi, Satoshi Tanaka
    ADVANCES IN SPACE RESEARCH 56(2) 341-354 2015年7月  
    Seismic data obtained over a broad frequency range are very useful in investigation of the internal structures of the Earth and other planetary bodies. However, planetary seismic data acquired through the NASA Apollo and Viking programs were obtained only over a very limited frequency range. To obtain effective seismic data over a broader frequency range on planetary surfaces, broadband seismometers suitable for planetary seismology must be developed. In this study, we have designed a new broadband seismometer based on a short-period seismometer whose resonant frequency is 1 Hz for future geophysical missions. The seismometer is of an electromagnetic type, light weight, small size and has good shock-durability, making it suitable for being loaded onto a penetrator, which is a small, hard-landing probe developed in the LUNAR-A Project, a previous canceled mission.We modified the short-period seismometer so as to have a flat frequency response above about 0.1 Hz and the detection limit could be lowered to cover frequencies below the frequency. This enlargement of the frequency band will allow us to investigate moonquakes for lower frequency components in which waveforms are less distorted because strong scattering due to fractured structures near the lunar surface is likely to be suppressed. The modification was achieved simply by connecting a feedback circuit to the seismometer, without making any mechanical changes to the short-period sensor. We have confirmed that the broadband seismometer exhibits the frequency response as designed and allows us to observe long-period components of small ground motions. Methods to improve the performance of the broadband seismometer from the current design are also discussed. These developments should promise to increase the opportunity for application of this small and tough seismometer in various planetary seismological missions. (C) 2015 COSPAR. Published by Elsevier Ltd. All rights reserved.
  • Ryuhei Yamada, Raphael F. Garcia, Philippe Lognonne, Naoki Kobayashi, Nozomu Takeuchi, Tanguy Nebut, Hiroaki Shiraishi, Marie Calvet, J. Ganepain-Beyneix
    PLANETARY AND SPACE SCIENCE 81 18-31 2013年6月  
    Information on the lunar central core; size, current state and composition; are key parameters to understand the origin and evolution of the Moon. Recent studies have indicated that possible seismic energies of core-reflected phases can be identified from past Apollo seismic data, and core sizes are determined, but we have still uncertainties to establish the lunar core parameters. We, therefore, plan to detect seismic phases that pass through the interior of the core and/or those reflected from the core-mantle boundary to ensure the parameters using new seismometers for future lunar soft-landing missions such as SELENE-2 and Farside Explorer projects.As the new seismometers, we can apply two types of sensors already developed; they are the Very Broad Band (VBB) seismometer and Short Period (SP) seismometer. We first demonstrate through waveform simulations that the new seismometers are able to record the lunar seismic events with S/N much better than Apollo seismometers. Then, expected detection numbers of core-phases on the entire lunar surface for the two types of seismometers are evaluated for two models of seismic moment distributions of deep moonquakes using the recent interior model (VPREMOON).The evaluation indicates that the VBB has performance to detect reflected S phases (ScS) from the core-mantle boundary mainly on the lunar near-side, and the P phases (PKP) passing through the interior of the core on some areas of the lunar far-side. Then, the SP can also detect PKP phases as first arrival seismic phase on limited regions on the lunar far-side. If appropriate positions of the seismic stations are selected, core-phases can be detected, allowing us to constrain the origin and evolution of the Moon with future lunar soft-landing missions. (C) 2013 Elsevier Ltd. All rights reserved.
  • R. Yamada, I. Yamada, H. Shiraishi, S. Tanaka, Y. Takagi, N. Kobayashi, N. Takeuchi, Y. Ishihara, H. Murakami, K. Yomogida, J. Koyama, A. Fujimura, H. Mizutani
    Planetary and Space Science 57(7) 751-763 2009年6月  査読有り
    We developed a seismometer system for a hard landing "penetrator" probe in the course of the former Japanese LUNAR-A project to deploy new seismic stations on the Moon. The penetrator seismometer system (PSS) consists of two short-period sensor components, a two-axis gimbal mechanism for orientation, and measurement electronics. To carry out seismic observations on the Moon using the penetrator, the seismometer system has to function properly in a lunar environment after a hard landing (impact acceleration of about 8000 G), and requires a signal-to-noise ratio to detect lunar seismic events. We evaluated whether the PSS could satisfactorily observe seismic events on the Moon by investigating the frequency response, noise level, and response to ground motion of our instrument in a simulated lunar environment after a simulated impact test. Our results indicate that the newly developed seismometer system can function properly after impact and is sensitive enough to detect seismic events on the Moon. Using this PSS, new seismic data from the Moon can be obtained during future lunar missions. © 2008 Elsevier Ltd. All rights reserved.
  • Satoshi Tanaka, Hiroaki Shiraishi, Manabu Kato, Tatsuaki Okada
    ADVANCES IN SPACE RESEARCH 42(2) 394-401 2008年7月  
    Further study for the planning of the post SELENE mission has been discussed by a dedicated working group. As the extension of the SELENE-B study [Okada, T., Sasaki, S., Sugihara, T., et al. Lander and rover exploration on the lunar surface: a study for SELENE-B mission. Adv. Space Res. 37, 88-92, 2006] which proposed in-situ geological investigations using a robotic rover and a static lander, this report newly proposes a revised configuration which enhances the scientific field of view. The spacecraft of this mission, "SELENE-II", is designed as a full payload of H-II launch vehicle, while the former study was designed as a half payload of the same vehicle. This expansion of capacity enabled us to increase the payload mass of the lander to deploy geophysical instruments and to land on a wider region on the Moon including polar regions. We also gained the opportunity to deploy two penetrators in order to make a wide network for geophysical observations. In the new configuration, this mission can install three stations of a global seismic network, which will be able to refine the deeper structure of the Moon. In this study also, a new type of deployment system, whose mechanical interface is much simpler than that of the LUNA R-A mission, is preliminarily designed.The selection of the landing site is still undergoing discussion, but the lander is required to operate as long as about one year and more for the geophysical observations, especially for seismology. In order to realize this, one possible idea is to land in permanently sunlit regions. Polar regions also have a benefit from the geological point of view; the north polar region is a typical high land area and the south one is a part of or adjacent to the South Pole Aitken (SPA), where the deeper part of the crust or the mantle material are expected to be collected.In addition to the lander scientific instruments designed previously (Okada et al., 2006.) for the geological survey, a broad band seismometer is considered to be deployed prior to other geophysical instruments and we expect it to provide us with information about the bulk layered structure with only one station if free oscillations are successfully detected. Even if the free oscillations cannot be detected, the dispersion of surface waves not affected by scattering of the regolith or megaregolith layer brings information to understand the crustal and upper mantle structures.Several landing missions are planned by NASA, CNSA, ISRO, and ESA by 2010-2015 during which the operational period is possible to be overlapped by the different missions. This must be a great opportunity to make larger network observations in the future. It must be a great opportunity to start international collaboration in various ways for the upcoming lunar exploration era. (c) 2007 COSPAR. Published by Elsevier Ltd. All rights reserved.

MISC

 22
  • 村上 英記, 小林 直樹, 白石 浩章, 田中 智, 早川 雅彦, 後藤 健, 石原 吉明, 山田 竜平, 川村 太一, 月内部構造探査WG
    日本惑星科学会秋期講演会予稿集 2014 "P2-36" 2014年9月10日  
  • 新谷 昌人, 小林 直樹, 白石 浩章
    Proceedings of the ISAS Lunar and Planetary Symposium 46 1-14,巻頭2p 2014年8月5日  
  • 白石 浩章, 山田 竜平, 小林 直樹
    宇宙科学技術連合講演会講演集 57 6p 2013年10月9日  
  • 白石 浩章, 小林 直樹, 早川 雅彦, 田中 智, 早川 基, 石井 信明, 小松 敬治
    日本惑星科学会秋期講演会予稿集 2012 19-19 2012年10月24日  
  • 小林 直樹, 白石 浩章, 小川 和律, 山田 竜平, 飯島 祐一, Nebut Tanguy, Raucourt Sebastein de, Bierwirth Marco, Reinhard Roll, Lognonne Philippe, 鹿熊 英昭, セレーネ2月広帯域地震計チーム
    日本惑星科学会秋期講演会予稿集 2012 105-105 2012年10月24日  
  • 新谷 昌人, 西川 泰弘, 堀 輝人, 小林 直樹, 白石 浩章, 鹿熊 英昭, 石原 吉明
    遊・星・人 : 日本惑星科学会誌 21(3) 289-293 2012年9月25日  
    地震観測は地球や惑星の内部構造を高い分解能で探査できる手段である.本稿は地下深部の高温環境や惑星表面の低温・高放射線環境など,極限環境における観測をめざした地震計開発について述べる.レーザ干渉計測を用いることにより,高い精度を維持したまま極限環境において動作できることが特徴である.プロトタイプを用いた性能評価では,1mHz〜5Hzの帯域で地上のLow Noise Modelの振動レベルが検知できる雑音性能であることを確認した.仮に火星表面に設置できれば,火星大気によって励起される常時自由振動の予想レベルを検知可能で,その固有周波数から火星のコアに対する制約が得られるかもしれない.
  • 白石 浩章, 山田 竜平, 石原 吉明, 小林 直樹, 鈴木 宏二郎, 田中 智
    遊・星・人 : 日本惑星科学会誌 21(3) 283-288 2012年9月25日  
    多点ネットワークを構成して火星表層環境および内部構造を観測するペネトレータミッションを提案する.現在の火星内部で生じているダイナミクスを反映する地震活動度と熱的状態を調査するとともに,地球型惑星の分化過程を反映する地殻-上部マントル構造と固体内部から表層および大気層への物質輸送過程に関する知見を得ることを目的とする.ペネトレータモジュールは突入速度300m/secで火星表層下2〜3mに潜り込むプローブ本体に,耐熱シールドと空力減速機構の役割をする膜面展開型柔構造エアロシェルを統合することで小型軽量なシステムを構成する.周回衛星から分離された4機のペネトレータは,火成活動の可能性が指摘されるElysium地域に最大300km間隔のネットワークを構成して地震観測や熱流量観測を行う.一方,柔構造エアロシェルには圧力計,温度計,磁力計,カメラを搭載して大気突入時のモニタリングを行う.
  • 藤村 彰夫, 田中 智, 白石 浩章
    月刊地球 34(4) 226-230 2012年4月  
  • 村上 英記, 田中 智, 小林 直樹, 白石 浩章, 早川 雅彦, 山田 竜平, 石原 靖, 岡元 太郎, 竹内 希, 早川 基, 月内部構造探査WG
    日本惑星科学会秋期講演会予稿集 2011 128-128 2011年10月23日  
  • 山田 竜平, 白石 浩章, 竹内 希, 小林 直樹, 田中 智, 村上 英記, 石原 靖, 岡元 太郎, 早川 雅彦, 早川 基, Garcia Raphael, Lognonne Philippe
    日本惑星科学会秋期講演会予稿集 2011 49-49 2011年10月23日  
  • 田中 智, 白石 浩章, 早川 基, 藤村 彰夫, 月内部構造探査ワーキンググループ
    遊・星・人 : 日本惑星科学会誌 20(3) 208-210 2011年9月25日  
    2007年2月にLUNAR-A計画が中止となってから4年が過ぎた.その間もペネトレータの開発を続け,最後の試験と臨んだ2010年8月のペネトレータの貫入衝撃認定試験にて耐衝撃技術の確立を無事確認することができた.LUNAR-A計画の中止の際に日本惑星科学会にはペネトレータ技術の有用性と計画中止後の開発継続を訴えていただいた.本報告書ではペネトレータを用いた月内部構造探査計画であったLUNAR-Aの中止の後,衝撃耐性技術の確立迄のペネトレータ開発の経緯を紹介する.また,本報告をもってペネトレータの開発に期待を寄せ辛抱強く応援していただいた日本惑星科学会の皆様への感謝の念を伝える.
  • 藤村 彰夫, 田中 智, 白石 浩章, 竹内 希
    日本地震学会ニュースレター : News letter 23(3) 44-46 2011年9月10日  
  • 小林 直樹, 白石 浩章, 村上 英記, 竹内 希, 岡元 太郎, 久家 慶子, 山田 竜平, 小川 和津, 鹿熊 英昭, 石原 靖, 荒木 英一郎, 趙 大鵬, 飯島 祐一, 川村 太一, 白井 慶, 田中 智, 早川 雅彦, 藤村 彰夫, 山田 功
    日本鉱物科学会年会講演要旨集 2011 17-17 2011年9月5日  
  • 田中 智, 川村 太一, 小林 直樹, 白石 浩章
    遊・星・人 : 日本惑星科学会誌 20(1) 4-10 2011年3月25日  
    弾性波による月内部構造の探査は残された月の起源,進化の謎にせまる上で最も効果的な手法の一つである.アポロミッションで得られた月震データから地殻-マントル境界やマントル速度構造など重要な知見が得られた.しかし月震データのクオリティーは十分なものではなく,走時データには研究者間の読み取りにばらつきがあり,結果が左右されている部分が多い.また,層境界を一意に同定できるほど波線の分布も十分ではない.アポロデータは現在もなお解析が続けられており,コアの存在などが示唆されているが確定的な証拠となるのは困難と考えられる.より広域のネットワーク観測や表層付近の散乱の影響を除去できる帯域での新たなる月震観測が切望され,その実現にむけた開発が始まっている.
  • NAKAMURA Akiko M., SHIRAISHI Hiroaki, HONDA Rie, IIJIMA Yu-ichi, HASHIMOTO Tatsuaki, NINOMIYA Keiken, YOKOTA Yasuhiro, SHIRAO Motomaro, TAKATA Toshiko, YAMAJI Atsushi, SASAKI Sho, OKADA Tatsuaki, MATSUNAGA Tsuneo, DEMURA Hirohide, HIRATA Naru, HONDA Chikatoshi, HARUYAMA Jun'ichi, OHTAKE Makiko, NODA Hirotomo, MIYAMOTO Hideaki, YOSHIKAWA Makoto, TSUCHIDA Satoshi, OHTAKI Toshiki, MURAKAMI Hideki, KOMORI Chosei, MASSON Phillippe, PINET Patrick, CHEVREL Serge D., DAYDOU Yves, HIRAMATSU Masaru
    宇宙航空研究開発機構研究開発報告 4 1-63 2005年3月  
    Lunar Imaging Camera (LIC) is a small, compact and lightweight monochromatic imager designed and developed for LUNAR-A, Japanese lunar mission. The scientific objectives of the camera address impact cratering, tectonic processes, volcanic features, and optical properties of the regolith surface.The image sensor is a linear CCD and is aligned with the spin axis of the spacecraft, which orbits the Moon at altitudes of 200-300 km. The two-dimensional image is taken using the spin motion of the spacecraft. The total field of view (FOV) of the camera is 360°(around the spin axis)×14.6°(along the CCD-array). LIC obtains an image in one spin. The angular resolution of the camera is about 20 arcsec/pixel at a spin rate of 3 rpm. The spatial resolution is about 25 m/pixels at the surface when the altitude is 250 km. The spin axis of the LUNAR-A approximately points toward the Sun, therefore, LIC can take images of the lunar surface with highly oblique illumination conditions near the terminator. A series of pre-flight tests of LIC was performed. In those tests, the hardware performance and the functions of LIC were verified and the data for radiometric and geometric corrections were obtained. This paper outlines the scientific objective, characteristics of LIC, the procedure and the results of the pre-flight tests and the operation plan of LIC.
  • Hiroaki SHIRAISHI, Satoshi TANAKA, Masahiko HAYAKAWA, Akio FUJIMURA, Hiroshi MIZUTANI
    The Institute of Space and Astronautical Science report 677 1-21 2000年3月  
    A hard landing probe "penetrator" has been thought to be a very useful tool for planetary exploration, because it provides cost-effective capability of deploying scientific instruments on planetary surface and subsurface. But development of the penetrator for planetary exploration requires better understanding penetration dynamics in geological materials. The present paper describes some experimental results on the penetrator dynamics obtained during the course of the development of the LUNAR-A penetrator. Special emphasis is placed on understanding the effect of the oblique incidence and the attack angle of the penetrator on penetration depth and a final attitude at the rest position. Many impact experiments into a simulated lunar surface material are made using penetrators 30 mm in diameter, and the penetration characteristics (penetration path length and inflection angle) are investigated as functions of impact velocity, penetrator shape, impact angle and attack angle. The results indicate that the torque applied to the penetrator in cases of the impact with a finite attack angle changes the penetration characteristics significantly. The experimental data also suggests that the impact angle does not have a substantial effect on penetration path length and that the truncation of the nose tip from a conical nose is efficient to stabilize the penetration orientation.
  • 白石 浩章
    日本惑星科学会秋期講演会予稿集 1997 71-71 1997年9月15日  
  • 早川 雅彦, 白石 浩章, 田中 智, 飯島 祐一, 藤村 彰夫, 水谷 仁, 山田 功夫, 小山 順二, 村上 英記, 石原 靖, 伊藤 潔, 須田 直樹, LUNAR-Aペネトレータサイエンスグループ
    日本惑星科学会秋期講演会予稿集 1996 58-58 1996年10月2日  
  • 白石 浩章, 田中 智, 早川 雅彦, 藤村 彰夫, 石井 信明, 水谷 仁, LUNAR-Aペネトレータ開発グループ
    日本惑星科学会秋期講演会予稿集 1996 59-59 1996年10月2日  
  • 田中智, 水谷仁, 藤村彰夫, 宝来帰一, 早川雅彦, 安部正真, 白石浩章, 平井研一
    日本惑星科学会秋季講演会予稿集 1996 60 1996年10月  
  • 白石 浩章, 田中 智, 早川 雅彦, 藤村 彰夫, 水谷 仁
    日本惑星科学会秋期講演会予稿集 1995 205-205 1995年11月13日  
    The accelerometer onboard LUNAR-A penetrator is developed to estimate the depth of emplacement and information on the physical properties of the lunar regolith. The decceleration record is also indispensable to design the structure of the outer case of lunar penetrator and to investigate quantitatively the shock-resistant capacity for the payload instruments. Investigation of several kinds of sensors' performance and improvement of the data acquisition system are made in order to design the most suitable accelerometer and its electronics for LUNAR-A penetrator. Using the piezoelectric type sensor with annular shear mode, the acceleration profiles with the sufficient accuracy are obtained under the actual flight conditions.
  • 水谷仁, 藤村彰夫, 早川雅彦, 田中智, 安部正真, 荒木博志, 白石浩章, 山田功夫
    科学衛星・宇宙観測シンポジウム 3rd 224-227 1994年10月  

所属学協会

 3

共同研究・競争的資金等の研究課題

 5