@Article{LopesIBVSCVM:2021:SiThMo,
               author = "Lopes, Andre Godoi and Irita, Ricardo Toshiyuki and Berni, Luiz 
                         Angelo and Vilela, Waldeir Amaral and Savonov, Graziela da Silva 
                         and Carlesso, Franciele and Vieira, Luis Eduardo Antunes and 
                         Miranda, Edson Luiz de",
          affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {Instituto 
                         Nacional de Pesquisas Espaciais (INPE)} and {Instituto Nacional de 
                         Pesquisas Espaciais (INPE)} and {Instituto Nacional de Pesquisas 
                         Espaciais (INPE)} and {Instituto Nacional de Pesquisas Espaciais 
                         (INPE)} and {Instituto Nacional de Pesquisas Espaciais (INPE)} and 
                         {Instituto Nacional de Pesquisas Espaciais (INPE)} and {Instituto 
                         Nacional de Pesquisas Espaciais (INPE)}",
                title = "Simplified Thermal Model for Absolute Radiometer Simulation",
              journal = "Journal of Solar Energy Engineering",
                 year = "2021",
               volume = "143",
                pages = "e051004",
             keywords = "absolute radiometer, thermal transfer, thermal sensor, thermal 
                         simulation, absorber, heat transfer, measurement, radiation, 
                         simulation, solar, space.",
             abstract = "The study of solar radiation in space has become something 
                         necessary, motivating the launch of radiometers on board 
                         satellites dedicated to perform total solar irradiance (TSI) 
                         measurements and to build a record of their behavior over the 
                         years, thus making these data essential for meteorology and 
                         climatology. In this study, we propose a simplified model to 
                         understand the thermal behavior of absolute radiometers, which are 
                         used in this type of measurement. The model considers the heat 
                         transfer among parts through conduction and loss only by radiation 
                         since the instrument operates in a space environment. The goal is 
                         to understand how each component interferes with sensitivity and 
                         response time of the instrument depending on its design, material, 
                         volume, and thermal contact. The model was applied to data 
                         generated by a prototype for validation.",
                  doi = "10.1115/1.4049939",
                  url = "http://dx.doi.org/10.1115/1.4049939",
                 issn = "0199-6231",
                label = "lattes: 9831996893882845 7 LopesIBVSCVM:2021:SiThMo",
             language = "en",
           targetfile = "lopes_simplified.pdf",
        urlaccessdate = "20 maio 2024"
}