HERMES CubeSat Payload Thermal Balance Test and Comparison with Finite Volume Thermal Model
HERMES CubeSat Payload Thermal Balance Test and Comparison with Finite Volume Thermal Model
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Basel: MDPI AG
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Language
English
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Basel: MDPI AG
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Contents
Scientific payloads onboard CubeSats usually have complex geometries and occasionally narrower allowed temperature ranges with respect to the rest of the spacecraft. In these cases, the capability to correctly predict the thermal behaviour of the payload once in orbit is mandatory. To achieve this ability, a thermal balance test is required to corr...
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HERMES CubeSat Payload Thermal Balance Test and Comparison with Finite Volume Thermal Model
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TN_cdi_doaj_primary_oai_doaj_org_article_d29d1e3a678b4ad68b00881b3fb58ad8
Permalink
https://devfeature-collection.sl.nsw.gov.au/record/TN_cdi_doaj_primary_oai_doaj_org_article_d29d1e3a678b4ad68b00881b3fb58ad8
Other Identifiers
ISSN
2076-3417
E-ISSN
2076-3417
DOI
10.3390/app13095452
