Planck Early Results. II. The thermal performance of Planck
Planck Collaboration: P. A. R. Ade, N. Aghanim, M. Arnaud, M. Ashdown,, J. Aumont, C. Baccigalupi, M. Baker, A. Balbi, A. J. Banday, R. B. Barreiro,, E. Battaner, K. Benabed, A. Benoit, J. P. Bernard, M. Bersanelli, P., Bhandari, R. Bhatia, J. J. Bock, A. Bonaldi, J. R. Bond

TL;DR
This paper reports on the thermal performance and cooling systems of the Planck space observatory, detailing how various passive and active cooling methods achieved the required low temperatures for scientific instruments.
Contribution
It provides a comprehensive description of the thermal design, cooling technologies, and temperature stability of the Planck spacecraft's instruments in space.
Findings
Achieved 93mK for HFI bolometer plate 50 days after launch.
Maintained stable temperatures with minimal impact on data quality.
Successfully integrated passive radiative and active cryogenic cooling systems.
Abstract
The performance of the Planck instruments in space is enabled by their low operating temperatures, 20K for LFI and 0.1K for HFI, achieved through a combination of passive radiative cooling and three active mechanical coolers. The scientific requirement for very broad frequency coverage led to two detector technologies with widely different temperature and cooling needs. Active coolers could satisfy these needs; a helium cryostat, as used by previous cryogenic space missions (IRAS, COBE, ISO, Spitzer, AKARI), could not. Radiative cooling is provided by three V-groove radiators and a large telescope baffle. The active coolers are a hydrogen sorption cooler (<20K), a 4He Joule-Thomson cooler (4.7K), and a 3He-4He dilution cooler (1.4K and 0.1K). The flight system was at ambient temperature at launch and cooled in space to operating conditions. The HFI bolometer plate reached 93mK on 3 July…
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