Small sensor probe for measuring plasma waves in space
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DOI[10.1186/s40623-015-0298-8]to the data of the same series
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- Material Type
- 記事
- Author/Editor
- Takahiro ZushiHirotsugu KojimaKeisuke Onishi
- Publication, Distribution, etc.
- Publication Date
- 2015-08-14
- Publication Date (W3CDTF)
- 2015-08-14
- Periodical title
- EPS : Earth, Planets and Space
- No. or year of volume/issue
- 67(127)
- Volume
- 67(127)
- ISSN (Periodical Title)
- 1880-5981
- ISSN-L (Periodical Title)
- 1343-8832
- Text Language Code
- eng
- DOI
- 10.1186/s40623-015-0298-8
- Persistent ID (NDL)
- info:ndljp/pid/9497201
- Collection
- Collection (Materials For Handicapped People:1)
- Collection (particular)
- 国立国会図書館デジタルコレクション > 電子書籍・電子雑誌 > その他
- Acquisition Basis
- オンライン資料収集制度
- Date Accepted (W3CDTF)
- 2015-09-15T20:13:28+09:00
- Date Captured (W3CDTF)
- 2015-08-20
- Format (IMT)
- application/pdf
- Access Restrictions
- 国立国会図書館内限定公開
- Service for the Digitized Contents Transmission Service
- 図書館・個人送信対象外
- Availability of remote photoduplication service
- 可
- Periodical Title (URI)
- Periodical Title (Persistent ID (NDL))
- info:ndljp/pid/9227920
- Data Provider (Database)
- 国立国会図書館 : 国立国会図書館デジタルコレクション
- Summary, etc.
- Background: Since conventional one-point observations of plasma phenomena in space cannot distinguish between time and spatial variations, the missions on the basis of multiple-point observations have become the trend. We propose a new system for multiple-point observation referred to as the monitor system for space electromagnetic environments (MSEE). Findings: The MSEE consists of small sensor probes that have a capability to measure electromagnetic waves and transfer received data to the central station through wireless communication. We developed the prototype model of the MSEE sensor probe. The sensor probe includes a plasma wave receiver, the microcontroller, the wireless communication module, and the battery in the 75-mm cubic housing. In addition, loop antennas, dipole antennas, and actuators that are used for expanding dipole antennas are attached on the housing. The whole mass of the sensor probe is 692 g, and the total power consumption is 462 mW. The sensor probe can work with both inner battery and external power supply. The maximum continuous operation time on battery power is more than 6 h. We verified the total performance for electric field measurements by inputting signal to preamplifier. In this test, we found that analog components had enough characteristics to measure electric fields, and the A/D conversion and the wireless transmission worked correctly. In the whole performance for electric fields, the sensor probe has equivalent noise level of - 135 dBV/m/√Hz. Conclusions: We succeed in developing the prototype model of the small sensor probe that had enough sensitivity for electric field to measure plasma waves and the ability to transfer observation data through wireless communication. The success in developing the small sensor probe for the measurement of plasma waves leads to the realization of the multiple-point observations using a lot of small probes scattered in space.
- DOI
- 10.1186/s40623-015-0298-8
- Access Restrictions
- インターネット公開
- Rights (production)
- © 2015 Zushi et al. This article is distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution, and reproduction in any medium, provided you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons license, and indicate if changes were made.
- Related Material (URI)
- Is Referenced By
- Development of an ASIC preamplifier for electromagnetic sensor probes for monitoring space electromagnetic environments
- References
- Tiny waveform receiver with a dedicated system chip for observing plasma waves in spaceThe THEMIS MissionHighly Sensitive Formaldehyde Gas Sensors Based on SnO<sub>2</sub>–ZnO NanocompositesCluster II: Plasma measurements in three dimensionsSCIFER‐Transverse ion acceleration and plasma wavesPlasma wave turbulence around the shuttle: Results from the Spacelab‐2 flightA Compact Loop Antenna System for Monitoring Local Electromagnetic Environments in Geospace
- Data Provider (Database)
- 国立情報学研究所 : CiNii Research
- Original Data Provider (Database)
- 学術機関リポジトリデータベース雑誌記事索引データベースCrossref科学研究費助成事業データベースCrossref
- Bibliographic ID (NDL)
- 9497201