Mechanical cooler system for the next-generation infrared space telescope SPICA
Mechanical cooler system for the next-generation infrared space telescope SPICA
复制标题
用于下一代红外太空望远镜 SPICA 的机械冷却系统
DOI:
10.1117/12.2232602
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发表时间:
2016
期刊:
影响因子:
--
通讯作者:
H. Shibai
中科院分区:
文献类型:
--
作者:
K. Shinozaki;H. Ogawa;T. Nakagawa;Yoichi Sato;H. Sugita;T. Yamawaki;T. Mizutani;H. Matsuhara;M. Kawada;A. Okabayashi;S. Tsunematsu;K. Narasaki;H. Shibai
The Space Infrared Telescope for Cosmology and Astrophysics (SPICA) is a pre-project of JAXA in collaboration with ESA to be launched in the 2020s. The SPICA mission is to be launched into a halo orbit around the second Lagrangian point in the Sun-Earth system, which allows us to use effective radiant cooling in combination with a mechanical cooling system in order to cool a 2.5m-class large IR telescope below 8K. Recently, a new system design in particular thermal structure of the payload module has been studied by considering the technical feasibility of a cryogenic cooled telescope within current constraints of the mission in the CDF (Concurrent Design Facility) study of ESA/ESTEC. Then, the thermal design of the mechanical cooler system, for which the Japanese side is responsible, has been examined based on the CDF study and the feasible solution giving a proper margin has been obtained. As a baseline, 4K / 1K-class Joule-Thomson coolers are used to cool the telescope and thermal interface for Focal Plane Instruments (FPIs). Additionally, two sets of double stirling coolers (2STs) are used to cool the Telescope shield. In this design, nominal operation of FPIs can be kept when one mechanical cooler is in failure.
DOI:
10.1117/12.2231613
发表时间:
2016
期刊:
Proceedings of the SPIE
影响因子:
--
作者:
Ogawa;H.; Nakagawa;T.; Matsuhara;H.; Shinozaki;K.; Goto;K.; Isobe;N.; Kawada;M.; Mizutani;T.; Sato;Y.; Sugita;H.; Takeuchi;S.; Yamawaki;T.; Shibai;H.
通讯作者:
H.