Thermal design utilizing radiative cooling for the payload module of LiteBIRD

Takashi Hasebe, Shingo Kashima, Satoru Uozumi, Hirokazu Ishino, Shin Utsunomiya, Hirofumi Noda, Kazuhisa Mitsuda, Yutaro Sekimoto, Tadayasu Dotani, Tomotake Matsumura, Hajime Sugai, Masahiro Tsujimoto, Hiroaki Imada, Masashi Hazumi

Research output: Chapter in Book/Report/Conference proceedingConference contribution

2 Citations (Scopus)

Abstract

The conceptual thermal design of the payload module (PLM) of LiteBIRD utilizing radiative cooling is studied. The thermal environment and structure design of the PLM strongly depend on the precession angle α of the spacecraft. In this study, the geometrical models of the PLM that consist of the sunshield, three layers of Vgrooves, and 5 K shield were designed in the cases of α = 45°, 30°, and 5°. The mission instruments of LiteBIRD are cooled down below 5 K. Therefore, heat transfers down to the 5 K cryogenic part were estimated in each case of α. The radiative heat transfers were calculated by using geometrical models of the PLM. The conductive heat transfers and the active cooling with cryocoolers were considered. We also studied the case that the inner surface of the V-groove is coated by a high-emissivity material.

Original languageEnglish
Title of host publicationSpace Telescopes and Instrumentation 2018
Subtitle of host publicationOptical, Infrared, and Millimeter Wave
EditorsGiovanni G. Fazio, Howard A. MacEwen, Makenzie Lystrup
PublisherSPIE
Volume10698
ISBN (Print)9781510619494
DOIs
Publication statusPublished - Jan 1 2018
EventSpace Telescopes and Instrumentation 2018: Optical, Infrared, and Millimeter Wave - Austin, United States
Duration: Jun 10 2018Jun 15 2018

Other

OtherSpace Telescopes and Instrumentation 2018: Optical, Infrared, and Millimeter Wave
CountryUnited States
CityAustin
Period6/10/186/15/18

Fingerprint

payloads
Cooling
modules
Heat transfer
cooling
Module
Heat Transfer
Cryocooler
Radiative Heat Transfer
V grooves
thermal environments
Cryogenics
Emissivity
radiative heat transfer
Spacecraft
emissivity
precession
conductive heat transfer
cryogenics
spacecraft

Keywords

  • CMB
  • LiteBIRD
  • Radiative cooling
  • Thermal design
  • V-grooves

ASJC Scopus subject areas

  • Electronic, Optical and Magnetic Materials
  • Condensed Matter Physics
  • Computer Science Applications
  • Applied Mathematics
  • Electrical and Electronic Engineering

Cite this

Hasebe, T., Kashima, S., Uozumi, S., Ishino, H., Utsunomiya, S., Noda, H., ... Hazumi, M. (2018). Thermal design utilizing radiative cooling for the payload module of LiteBIRD. In G. G. Fazio, H. A. MacEwen, & M. Lystrup (Eds.), Space Telescopes and Instrumentation 2018: Optical, Infrared, and Millimeter Wave (Vol. 10698). [1069864] SPIE. https://doi.org/10.1117/12.2313034

Thermal design utilizing radiative cooling for the payload module of LiteBIRD. / Hasebe, Takashi; Kashima, Shingo; Uozumi, Satoru; Ishino, Hirokazu; Utsunomiya, Shin; Noda, Hirofumi; Mitsuda, Kazuhisa; Sekimoto, Yutaro; Dotani, Tadayasu; Matsumura, Tomotake; Sugai, Hajime; Tsujimoto, Masahiro; Imada, Hiroaki; Hazumi, Masashi.

Space Telescopes and Instrumentation 2018: Optical, Infrared, and Millimeter Wave. ed. / Giovanni G. Fazio; Howard A. MacEwen; Makenzie Lystrup. Vol. 10698 SPIE, 2018. 1069864.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Hasebe, T, Kashima, S, Uozumi, S, Ishino, H, Utsunomiya, S, Noda, H, Mitsuda, K, Sekimoto, Y, Dotani, T, Matsumura, T, Sugai, H, Tsujimoto, M, Imada, H & Hazumi, M 2018, Thermal design utilizing radiative cooling for the payload module of LiteBIRD. in GG Fazio, HA MacEwen & M Lystrup (eds), Space Telescopes and Instrumentation 2018: Optical, Infrared, and Millimeter Wave. vol. 10698, 1069864, SPIE, Space Telescopes and Instrumentation 2018: Optical, Infrared, and Millimeter Wave, Austin, United States, 6/10/18. https://doi.org/10.1117/12.2313034
Hasebe T, Kashima S, Uozumi S, Ishino H, Utsunomiya S, Noda H et al. Thermal design utilizing radiative cooling for the payload module of LiteBIRD. In Fazio GG, MacEwen HA, Lystrup M, editors, Space Telescopes and Instrumentation 2018: Optical, Infrared, and Millimeter Wave. Vol. 10698. SPIE. 2018. 1069864 https://doi.org/10.1117/12.2313034
Hasebe, Takashi ; Kashima, Shingo ; Uozumi, Satoru ; Ishino, Hirokazu ; Utsunomiya, Shin ; Noda, Hirofumi ; Mitsuda, Kazuhisa ; Sekimoto, Yutaro ; Dotani, Tadayasu ; Matsumura, Tomotake ; Sugai, Hajime ; Tsujimoto, Masahiro ; Imada, Hiroaki ; Hazumi, Masashi. / Thermal design utilizing radiative cooling for the payload module of LiteBIRD. Space Telescopes and Instrumentation 2018: Optical, Infrared, and Millimeter Wave. editor / Giovanni G. Fazio ; Howard A. MacEwen ; Makenzie Lystrup. Vol. 10698 SPIE, 2018.
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