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The ISO-Cryostat, it's Current Status and Early Test Results
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English
Abstract
The ISO-satellite consists of a Service and a Payload Module, the latter being essentially made up of the Cryostat. The present paper describes the current status of this cryostat. The general structural and thermal layout, the He-flow schematic and safety system and the general cover layout are described together with an overview on the existing hardware. Some first test results are as well reported.
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Citation
Seidel, A. and Passvogel, T., "The ISO-Cryostat, it's Current Status and Early Test Results," SAE Technical Paper 901340, 1990, https://doi.org/10.4271/901340.Also In
References
- “The Current ISO-Cryostat Design” Seidel A. Wanner M. Davidson A.M. Proc. 12 th Intern. Cryogenic Engineering Conf. July 12 - 15 1988
- “Directly Operated Valve for Space Cryostat” Fuchs F. Seidel A. Cryogenics 27 Jan. 1987
- “Direct Liquid Content Measurement Applicable for Hell-Space Cryostat” Wanner M. Advances in Cryogenic Engineering 33 917
- “Very Low Force Cooling Contacts for the ISO-Cryostat Cover” Schaellig R. Seidel A. Space Cryogenics Workshop July 30 Aug. 1 1989 Cryogenics