| Project/Area Number |
19204017
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| Research Category |
Grant-in-Aid for Scientific Research (A)
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| Allocation Type | Single-year Grants |
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| Section | 一般 |
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| Research Field |
Astronomy
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| Research Institution | Tokyo Institute of Technology |
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Principal Investigator |
KATAOKA Jun Tokyo Institute of Technology, 理工学術院, 准教授 (90334507)
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| Co-Investigator(Kenkyū-buntansha) |
MATSUNAGA Saburo 東京工業大学, 大学院・理工学研究科, 准教授 (00222307)
河合 誠之 東京工業大学, 大学院・理工学研究科, 教授 (80195031)
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| Co-Investigator(Renkei-kenkyūsha) |
KAWAI Nobuyuki 東京工業大学, 大学院・理工学研究科, 教授 (80195031)
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| Project Period (FY) |
2007 – 2009
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| Project Status |
Completed (Fiscal Year 2009)
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| Budget Amount *help |
¥45,760,000 (Direct Cost: ¥35,200,000、Indirect Cost: ¥10,560,000)
Fiscal Year 2009: ¥14,820,000 (Direct Cost: ¥11,400,000、Indirect Cost: ¥3,420,000)
Fiscal Year 2008: ¥15,990,000 (Direct Cost: ¥12,300,000、Indirect Cost: ¥3,690,000)
Fiscal Year 2007: ¥14,950,000 (Direct Cost: ¥11,500,000、Indirect Cost: ¥3,450,000)
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| Keywords | X線γ線天文学 / 小型大学衛星 / 散乱偏光計 / 突発天体 / ガンマ線バースト / CMG / 硬X線天文学 |
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| Research Abstract |
We developed an engineering system for a small satellite TSUBMAME, the 4^<th> university satellite of 50kg in mass, developed by the Tokyo Tech. The mission will be an important pathfinder for future space science using the small satellites. We constructed engineering test modules for the hard X-ray Compton polarimeter, wideband burst monitor as well as high-speed attitude control system based on the control momentum gyro. We showed that all the system works pretty well to achieve our science goals for detecting hard X-ray/gamma-ray polarization in various transient sources.
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