Thermal Design of SPICA cryogenic cooling system

Abstract

This paper presents a thermal design of a cryogenic cooling system for the Space Infrared Telescope for Cosmology and Astrophysics (SPICA), which is an infrared astronomy mission with a 2.5-m telescope. SPICA is a joint space mission between ESA and JAXA and was one of the three candidates for the ESA's Cosmic Vision Medium Class M5 mission. One of the challenging tasks of SPICA is to cool the telescope and all instruments to cryogenic temperature, below 8 K, for highly sensitive, high-resolution observations. Two possible configurations, the vertical and the horizontal ones, were proposed for SPICA, and the vertical configuration was chosen mainly from system points of view. This paper discusses the potential difficulties in thermal design with particular emphasis on the vertical configuration compared to the horizontal configuration. We show the latest thermal design and the steady-state thermal analysis results especially for the vertical configuration.

Description

Masaru Saijo, Japan Aerospace Exploration Agency
Takao Nakagawa, Japan Aerospace Exploration Agency
Hiroyuki Ogawa, Japan Aerospace Exploration Agency
Keisuke Shinozaki, Japan Aerospace Exploration Agency
Kenichiro Sawada, Japan Aerospace Exploration Agency
Hideo Matsuhara, Japan Aerospace Exploration Agency
Chihiro Tokoku, Japan Aerospace Exploration Agency
Toyoaki Suzuki, Japan Aerospace Exploration Agency
Naoki Isobe, Japan Aerospace Exploration Agency
ICES108: Thermal Control of Cryogenic Instruments and Optical Systems
The 50th International Conference on Environmental Systems was held virtually on 12 July 2021 through 14 July 2021.

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Keywords

Infrared telescope, Cryogenic thermal design, Thermal control system

Citation