The required lifetime for the Astro-E X-Ray Spectrometer (XRS) is 2 years, with a goal of 2.5 years. To meet this requirement, significant advances in state-of-the-art longlife cryogenic systems are required. The XRS system is a hybrid neon/helium system with a final stage of cooling provided by an
Design and performance of the HESSI cryostat
โ Scribed by R Boyle; S Banks; P Cleveland; P Turin
- Book ID
- 104112538
- Publisher
- Elsevier Science
- Year
- 1999
- Tongue
- English
- Weight
- 648 KB
- Volume
- 39
- Category
- Article
- ISSN
- 0011-2275
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โฆ Synopsis
The High Energy Solar Spectroscopic Imager (HESSI) spacecraft, to be launched in July 2000, will be used to observe the Sun with the ยฎnest angular and energy resolutions ever achieved from a few keV to hundreds of keV. The spacecraft will use an array of nine germanium (Ge) detectors, each 7.1 cm in diameter and 8.5 cm long, operating at 75 K. The detectors are mounted in a cryostat on a common coldplate, and cooled by a small Stirling-cycle cryocooler. This paper describes the design of the cryostat, special accommodations for the Ge detectors, interfaces with the cryocooler, and thermal performance of the engineering test unit.
๐ SIMILAR VOLUMES
The effect of the conductive heat transfer for a cooled shield and convective heat transfer from the shield to the cooling vapour upon the heat flow through a cryostat insulation is studied.