研究者業績
基本情報
論文
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Space Telescopes and Instrumentation 2024: Optical, Infrared, and Millimeter Wave 9-9 2024年8月23日
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Modeling, Systems Engineering, and Project Management for Astronomy XI 93-93 2024年8月23日
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Proceedings of SPIE - The International Society for Optical Engineering 13092 2024年Structural, Thermal and Optical Performance (STOP) analysis is performed to investigate the stability of the telescope to be onboard the Japan Astrometry Satellite Mission for INfrared Exploration (JASMINE). In order to perform one of the prime science objectives, high-precision astrometric observations in the wavelength range of 1.0–1.6 µm toward the Galactic center to reveal its central core structure and formation history, the JASMINE telescope is requested to be highly stable with an orbital change in the image distortion pattern being less than a few 10 µas after low-order correction. The JASMINE telescope tried to satisfy this requirement by adopting two design concepts. Firstly, the mirror and their support structures are made of extremely low coefficient-of-thermal-expansion materials. Secondly, their temperatures are highly stabilized with an orbital variation of less the 0.1 ◦C by the unique thermal control idea. Through the preliminary STOP analysis, the structural and thermal structural feasibility of the JASMINE telescope is considered. By combining the results of the structural and thermal design, its thermal deformation is estimated. The optical performance of the JASMINE telescope after the thermal deformation is numerically evaluated. It is found that the thermal displacement of the mirrors in the current structural thermal design produces a slightly large focus-length change. As far as the focus adjustment is adequately applied, the orbital variation of the image distortion pattern is suggested to become acceptable after the low-order correction.
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Proceedings of SPIE, Ground-based and Airborne Instrumentation for Astronomy IX 12184 2022年8月29日MIMIZUKU is the first-generation mid-infrared instrument for the TAO 6.5-m telescope. It has three internal optical channels to cover a wide wavelength range from 2 to 38 mu m. Of the three channels, the NIR channel is responsible for observations in the shortest wavelength range, shorter than 5.3 mu m. The performance of the NIR channel is evaluated in the laboratory. Through the tests, we confirm the followings: 1) the detector (HAWAII-1RG with 5.3-mu m cutoff) likely achieves similar to 80% quantum efficiency; 2) imaging performance is sufficient to achieve seeing-limit spatial resolution; 3) system efficiencies in imaging modes are 2.4-31%; and 4) the system efficiencies in spectroscopic modes is 5-18%. These results suggest that the optical performance of the NIR channel is achieved as expected from characteristics of the optical components. However, calculations of the background levels and on-sky sensitivity based on these results suggest that neutral density (ND) filters are needed to avoid saturation in L'- and M'-band observations and that the ND filters and the entrance window, made of chemical-vapor-deposition (CVD) diamond, significantly degrade the sensitivity in these bands. This means that the use of different window materials and improvements of the detector readout speed are required to achieve both near-infrared and long-wavelength mid-infrared (>30 mu m) observations.
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Millimeter, Submillimeter, and Far-Infrared Detectors and Instrumentation for Astronomy X 11453 2020年12月18日We have developed a prototype half-wave plate (HWP) based polarization modulator (PMU) for Cosmic Microwave Background polarization measurement experiments. We built a 1/10 scaled PMU that consists of a 50 mm diameter five-layer achromatic HWP with a moth-eye broadband anti-reflection sub-wavelength structure mounted on a superconducting magnetic bearing. The entire system has cooled below 20 K in a cryostat chamber that has two millimeter-wave transparent windows. A coherent source and the diode detector are placed outside of the cryostat and the millimeter-wave goes through the PMU in the cryostat. We have measured the modulated signal by the PMU, analyzed the spectral signatures, and extracted the modulation efficiency over the frequency coverage of 34-161 GHz. We identified the peaks in the optical data, which are synchronous to the rotational frequency. We also identified the peaks that are originated from the resonance frequency of the levitating system. We also recovered the modulation efficiency as a function of the incident electromagnetic frequency and the data agrees to the predicted curves within uncertainties of the input parameters, i.e.The indices of refraction, thickness, and angle alignment. Finally, we discuss the implication of the results when this is applied to the LiteBIRD low-frequency telescope.
MISC
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The Institute of Space and Astronautical Science report. S.P. 14 281-288 2000年12月The Infrared Camera (IRC) is one of the focal-plane instruments on board ASTRO-F(also called as the Infrared Imaging Surveyor; IRIS) and will make imaging and low-resolutionspectroscopy observations over a wide spectral range in the near- to mid-infrared from 2 - 26μm.The IRC will be operated in the pointed observation mode of ASTRO-F to make deep photometricand spectroscopic surveys of wide field-of-views. It will provide a significant database for studiesof the formation and evolution of galaxies, properties of brown dwarfs, evolution of planetarysystems, and processes of star formation. The IRC comprises three channels: NIR (2 - 5μm),MIR-S (5 - 12μm) and MIR-L (12 - 26μm), and employs state-of-the-art large format arraydetectors. The NIR channel uses a 512×412 InSb array and the MIR channels adopt 256×256Si:As impurity band conduction (IBC) arrays. Each channel has a field-of-view of 10′×10′with anearly diffraction-limited spatial resolution. The NIR and MIR-S channels simultaneously observethe same field on the sky, while the MIR-L observes the sky about 200 away from the NIR/MIR-Sposition. The design overview and current development status of the IRC are presented.
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ASTROPHYSICAL JOURNAL 427(1) 511-518 1994年5月We have developed a Fabry-Perot imager at the Nasmyth focus of the Communications Research Laboratory (CRL) 1.5 m telescope. The field of view of the camera is 4'.0 x 4'.0, which is the largest among near-infrared Fabry-Perot imagers. In order to make the velocity shift in the field of view small, we chose a long focal length for the collimator (approximately 470 mm). The accurate parallelism of reflecting surfaces, 5 nm, is achieved by systems including a He-Ne laser and Si photodiodes. This gives an effective finesse of approximately 50. Wavelength calibration is carried out by using a Kr lamp. This calibration includes a correction for wavelength-dependent phase changes in the reflective coatings of the etalon. Using this Fabry-Perot imager, we obtained Brgamma and Pabeta images of the Orion Nebula, including the Bright Bar and a part of the Trapezium. From these images we obtained the distribution of extinction in this area. We found that there are regions with a tendency for the Brgamma/Pabeta intensity ratio to be larger at a place with a larger Brgamma intensity. We conclude that in such regions dust grains exist within the ionized region, causing the extinction.
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ASTROPHYSICAL JOURNAL 420(2) 746-755 1994年1月A continuum-subtracted image of the H-2 v=1-0 S(1) line covering the central 4' square portion of the Orion-KL region, has been obtained using a wide-field Fabry-Perot imager at the Communications Research Laboratory 1.5 m telescope. Nine H-2 peaks (including four newly identified) are found in the core, as well as a curved, bridgelike structure that encroaches on the inner edge of the disk structure observed in CS (J = 1-0) emission. This existence of the bridge indicates that the outflow from IRc2 occurs not only toward the bipolar axis but also toward the disk, and suggests channeling by the disk of a more or less isotropic flow from IRc2 into a bipolar flow. Outside the core, where finger-like features of H-2 emission are seen, we identify 43 hot H-2 clumps. These are located along filamentary structures seen in CS (J = 1-0) maps and avoid peaks of CS intensity. The geometrical thickness of the hot H-2 in these features is much smaller than their typical dimensions. We conclude that the H-2 emission from the clumps is radiated at the surfaces of the CS filaments, implying that outflow from IRc2 shocks the H-2 at the surfaces. From comparison of polarization measurements of Burton et al. (1991) with the present measurements, as well as from discussion of the energetics, we rule out the possibility that the H-2 clumps are due to reflection.
共同研究・競争的資金等の研究課題
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日本学術振興会 科学研究費助成事業 2014年4月 - 2018年3月
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日本学術振興会 科学研究費助成事業 2011年4月 - 2016年3月
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日本学術振興会 科学研究費助成事業 2007年 - 2010年
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日本学術振興会 科学研究費助成事業 2007年 - 2008年
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日本学術振興会 科学研究費助成事業 2004年 - 2008年