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 宇宙機応用工学研究系 准教授
- 学位
- 工学博士(東京大学)
- J-GLOBAL ID
- 200901062630747582
- researchmap会員ID
- 1000292029
研究キーワード
12研究分野
4経歴
2受賞
2論文
81-
Proceedings of 34th International Symposium on Space Technology and Science ISTS 2023-j-13 2023年6月 査読有り最終著者
-
Publications of Astronomical Society of Japan 75(3) 567-583 2023年3月 査読有りWe built a Ka-band dual-circular-polarization low-noise receiver for the Misasa 54 m parabola antenna in Misasa, Japan. The antenna is designed to be combined with a transmitter and receiver system at the X band (around 8 GHz) and simultaneously with a receiver system at the Ka band. The Ka band is the frequency band around 30 GHz, which is important for deep-space communications and radio astronomy. The receiver comprises some waveguide components including a feed horn, a circular polarizer, and low-noise amplifiers. The components are installed in a vacuum vessel and are cooled to 4 K with a Gifford-McMahon refrigerator, providing low-noise performance. The receiver is capable of simultaneously handling the left- and right-hand circular-polarization (LHCP and RHCP) channels. The receiver-noise temperature was measured to be T-RX similar or equal to 14 K in both the LHCP and RHCP channels. The system-noise temperature, including the antenna loss and atmospheric attenuation at the zenith, was measured to be T-sys = 36-37 K in both the LHCP and RHCP channels on a clear day in September at Misasa. When the receiver is used with the X-band transmitter, the system-noise temperature is maintained at T-sys similar or equal to 42 K in the RHCP channel. The degradation in the system-noise temperature is attributed to a frequency-selective reflector, which divides the signals in the X and Ka bands. There is no contamination from the transmitter to damage the receiver. The receiver has already been in use for deep-space communications and radio-astronomy observations. Our team in the radio-astronomy laboratory of ISAS/JAXA is responsible for the development of the receiver and the measurements of its performance.
-
Hayabusa2 Asteroid Sample Return Mission 453-475 2022年
-
Astronomy and Astrophysics 647 2021年3月1日A projectile accelerated by the Hayabusa2 Small Carry-on Impactor successfully produced an artificial impact crater with a final apparent diameter of 14.5 ± 0.8 m on the surface of the near-Earth asteroid 162173 Ryugu on April 5, 2019. At the time of cratering, Deployable Camera 3 took clear time-lapse images of the ejecta curtain, an assemblage of ejected particles forming a curtain-like structure emerging from the crater. Focusing on the optical depth of the ejecta curtain and comparing it with a theoretical model, we infer the size of the ejecta particles. As a result, the typical size of the ejecta particles is estimated to be several centimeters to decimeters, although it slightly depends on the assumed size distribution. Since the ejecta particles are expected to come from a depth down to ∼1 m, our result suggests that the subsurface layer of Ryugu is composed of relatively small particles compared to the uppermost layer on which we observe many meter-sized boulders. Our result also suggests a deficit of particles of less than ∼1 mm in the subsurface layer. These findings will play a key role in revealing the formation and surface evolution process of Ryugu and other small Solar System bodies.
MISC
104担当経験のある科目(授業)
1-
宇宙情報工学 (総合研究大学院大学)
共同研究・競争的資金等の研究課題
6-
文部科学省 科学研究費補助金(基盤研究(B)) 2005年 - 2007年
-
日本学術振興会 科学研究費助成事業 2005年 - 2007年
-
文部科学省 科学研究費補助金(若手研究(B)) 2003年 - 2004年
-
文部科学省 科学研究費補助金(基盤研究(A)) 2002年 - 2004年
-
文部科学省 科学研究費補助金(奨励研究(A), 若手研究(B)) 2001年 - 2002年