Preliminary structural design and key technology demonstration of cryogenic assembly in the next-generation infrared space telescope SPICA

Author:

Mizutani Tadahito1,Yamawaki Toshihiko1,Komatsu Keiji2,Goto Ken2,Takeuchi Shinsuke2,Shinozaki Keisuke1,Matsuhara Hideo2,Nakagawa Takao2

Affiliation:

1. Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency, Tsukuba Space Center, 2-1-1 Sengen, Tsukuba-shi, Ibaraki 305-8505, Japan

2. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, 3-1-1 Yoshinodai, Chuo-ku, Sagamihara-shi, Kanagawa 252-5210, Japan

Publisher

SPIE-Intl Soc Optical Eng

Subject

Space and Planetary Science,Mechanical Engineering,Astronomy and Astrophysics,Instrumentation,Control and Systems Engineering,Electronic, Optical and Magnetic Materials

Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Cryogenic system of the infrared space mission SPICA;Space Telescopes and Instrumentation 2020: Optical, Infrared, and Millimeter Wave;2020-12-13

2. Thermal and mechanical design of SPICA payload module;Space Telescopes and Instrumentation 2018: Optical, Infrared, and Millimeter Wave;2018-07-24

3. SPICA—A Large Cryogenic Infrared Space Telescope: Unveiling the Obscured Universe;Publications of the Astronomical Society of Australia;2018

4. Trade-off studies on LiteBIRD reflectors;Material Technologies and Applications to Optics, Structures, Components, and Sub-Systems III;2017-09-05

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