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The Design and Testing of the ISO-Payload Module
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English
Abstract
The ISO-satellite consists of a Service and a Payload Module (PLM), the latter being essentially made up of the Cryostat. The paper describes essentially the hardware status of the PLM-flight model as it is delivered for final satellite integration and acceptance testing before flight. The various test activities and essential results obtained during development, qualification and PLM-flight model acceptance up to delivery to ESTEC are summarized.
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Citation
Paβvogel, T., Seidel, A., Wilz, E., and Sagner, U., "The Design and Testing of the ISO-Payload Module," SAE Technical Paper 941274, 1994, https://doi.org/10.4271/941274.Also In
References
- Seidel A. Paβvogel Th. “The ISO-Cryostat; Its Qualification Status” Advances in Cryogenic Engineering 37 1327
- Seidel A. Wanner M. Davidson A. M. “The Current ISO-Cryostat Design” Proc. 12th Intern. Cryogenic Engineering Conf. July 12 - 15 1988
- Fuchs F. Seidel A. “Directly Operated Valve for Space Cryostat” Cryogenics 27 Jan. 1987
- Wanner M. “Direct Liquid Content Measurement Applicable for Hell-Space Cryostat” Advances in Cryogenic Engineering 33 917
- Schaellig R. Seidel A. “Very Low Force Cooling Contacts for the ISO-Cryostat Cover” Cryogenics 30 March 1990