The Design and Testing of the ISO-Payload Module 941274
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.
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. Download Citation
Author(s):
Th. Paβvogel, A. Seidel, E. Wilz, U. Sagner
Affiliated:
Deutsche Aerospace
Pages: 16
Event:
International Conference On Environmental Systems
ISSN:
0148-7191
e-ISSN:
2688-3627
Also in:
SAE 1994 Transactions: Journal of Aerospace-V103-1
Related Topics:
Hardware
Satellites
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