Design of a Deployable Helix Antenna at L-Band for a 1-Unit CubeSat: From Theoretical Analysis to Flight Model Results

The [Formula: see text] Cat-4 mission aims at demonstrating the capabilities of a CubeSat to perform Earth Observation (EO) by integrating a combined GNSS-R and Microwave Radiometer payload into a 1-Unit CubeSat. One of the greatest challenges is the design of an antenna that respects the 1-Unit Cub...

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Detalles Bibliográficos
Autores principales: Fernandez, Lara, Sobrino, Marco, Ruiz-de-Azua, Joan Adria, Calveras, Anna, Camps, Adriano
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2022
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9144964/
https://www.ncbi.nlm.nih.gov/pubmed/35632038
http://dx.doi.org/10.3390/s22103633

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9144964/
https://www.ncbi.nlm.nih.gov/pubmed/35632038
http://dx.doi.org/10.3390/s22103633

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