The 3Cat-4 Spacecraft Thermal Analysis and Thermal Vacuum Test Campaign Results

3Cat-4 is the fourth member of the CubeSat series of UPC’s NanoSat Lab, and it was selected by the ESA Academy’s Fly Your Satellite! program in 2017. This mission aims at demonstrating the capabilities of nano-satellites, and in particular those based in the 1-Unit CubeSat standard, for challenging Earth Observation (EO) using Global Navigation Satellite System-Reflectometry (GNSS-R) and L-band microwave radiometry, as well as for Automatic Identification Systems (AIS). The following study presents the results of the thermal analysis carried out for this mission, evaluating different scenarios, including the most critical cases at both high and low temperatures. The results consider different albedos and orbital parameters in order to establish the optimal temperatures to achieve the best mission performance within the nominal temperatures, and in all operational modes of the satellite. Simulation results are included considering the thermal performance of other materials, such as Kapton, as well as the redesign of the optical properties of the satellite’s solar panels. The correlation with the thermal model and the TVAC test campaign was conducted at the ESA ESEC-GALAXIA facilities in Belgium.

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Publication Details

Journal
Aerospace
Published
2024-09-30
DOI
https://doi.org/10.3390/aerospace11100805
Citations
7
Primary Topic
Spacecraft Design and Technology
Type
article
Field-Weighted Citation Impact
9.09

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article

The 3Cat-4 Spacecraft Thermal Analysis and Thermal Vacuum Test Campaign Results

David Palma, Inés Terraza Palanca, Lily Ha, Jeimmy Nataly Buitrago-Leiva et al.
7 citations
Aerospace
Spacecraft Design and Technology
9.09
article

The 3Cat-4 Spacecraft Thermal Analysis and Thermal Vacuum Test Campaign Results

David Palma, Inés Terraza Palanca, Lily Ha, Jeimmy Nataly Buitrago-Leiva, Małgorzata Sołyga, Lara Fernandez, Adriano Camps, Luis Contreras-Benito, Guillem Gracia-Sola, Cristina del Castillo Sancho
article en
7 citations

Abstract

3Cat-4 is the fourth member of the CubeSat series of UPC’s NanoSat Lab, and it was selected by the ESA Academy’s Fly Your Satellite! program in 2017. This mission aims at demonstrating the capabilities of nano-satellites, and in particular those based in the 1-Unit CubeSat standard, for challenging Earth Observation (EO) using Global Navigation Satellite System-Reflectometry (GNSS-R) and L-band microwave radiometry, as well as for Automatic Identification Systems (AIS). The following study presents the results of the thermal analysis carried out for this mission, evaluating different scenarios, including the most critical cases at both high and low temperatures. The results consider different albedos and orbital parameters in order to establish the optimal temperatures to achieve the best mission performance within the nominal temperatures, and in all operational modes of the satellite. Simulation results are included considering the thermal performance of other materials, such as Kapton, as well as the redesign of the optical properties of the satellite’s solar panels. The correlation with the thermal model and the TVAC test campaign was conducted at the ESA ESEC-GALAXIA facilities in Belgium.

AerospaceVol. 11(10)
United Arab Emirates University (AE), Institut d'Estudis Espacials de Catalunya (ES), FC Barcelona (ES), European Space Research and Technology Centre (NL), Universitat Politècnica de Catalunya (ES)
European Regional Development Fund, Agencia Estatal de Investigación
Openalex Percentile: Top 3%
Spacecraft Design and Technology
9.09
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