| Project/Area Number |
16340149
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| Research Category |
Grant-in-Aid for Scientific Research (B)
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| Allocation Type | Single-year Grants |
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| Section | 一般 |
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| Research Field |
Space and upper atmospheric physics
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| Research Institution | Japan Aerospace Exploration Agency |
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Principal Investigator |
HAYAKAWA Hajime Japan Aerospace Exploration Agency, Institute of Snace and Astronautical Science, Professor, 宇宙科学研究本部・固体惑星科学研究系, 教授 (90167594)
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| Co-Investigator(Kenkyū-buntansha) |
SAITO Yoshifumi Japan Aerospace Exploration Agency, Institute of Space and Astronautical Science, Associate Professor, 宇宙科学研究本部・宇宙プラズマ研究系, 助教授 (30260011)
ASAMURA Kazushi Japan Aerospace Exploration Agency, Institute of Space and Astronautical Science, Research Associate, 宇宙科学研究本部・宇宙プラズマ研究系, 助手 (50321568)
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| Project Period (FY) |
2004 – 2005
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| Project Status |
Completed (Fiscal Year 2005)
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| Budget Amount *help |
¥16,500,000 (Direct Cost: ¥16,500,000)
Fiscal Year 2005: ¥6,600,000 (Direct Cost: ¥6,600,000)
Fiscal Year 2004: ¥9,900,000 (Direct Cost: ¥9,900,000)
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| Keywords | Velocity Distribution Function / Instrument / Mass Spectrometry / Upper Atmosphere |
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| Research Abstract |
Neutral Mass and velocity Spectrometer (NMS) is one of the e-POP (enhanced Polar Outflow Probe) payload instruments on a Canadian small satellite CASSIOPE which will be launched in the end of 2007. NMS measures density and 2-dimensional velocity distribution function of each major neutral species such as H_2, He, O, and N_2 in the upper atmosphere using 2-D position detection. The velocity distribution function of neutral atmospheric species has never been measured: However the information of the velocity distribution is important to understand the behavior of nonthermal components of the upper atmosphere, which are considered to be generated by various collisional processes among ambient neutral species and high-energy plasmas. Basic design of NMS instrument has been done and its feasibility has been confirmed experimentally. We modified the measurement method to adapt to the actual flight experiment, which has limited resources relative to the laboratory environment. Neutral particles enter the NMS instrument with spacecraft ram velocity and ionized by an electron gun, then introduced to a chamber behind the electron beam. In the chamber the ions are accelerated towards the bottom in the perpendicular direction to the ram velocity by a pulsed negative voltage applied to the top plate of the chamber. A part of ions reach a slit in the bottom of the chamber and enter the ion acceleration region where ions are accelerated by a constant uniform electric field to a detector. Through this process, acceleration of incident particle occurs only in a direction perpendicular to the ram and incident velocity in ram plain is maintained. The detector consists of a Micro Channel Plate (MCP) and a position sensitive anode. An accelerated ion arrives at a position according to its mass and velocity. The distribution of detected positions represents 2-D velocity distribution function of neutral particles.
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