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@InProceedings{SantosBGBMKCCR:2014:TUHePi,
               author = "Santos, Nadjara dos and Bertoldo J{\'u}nior, Jorge and Genaro, 
                         Gino and Batista Neto, Jos{\'e} Ant{\^o}nio and Mendes, Geraldo 
                         Orlando and Kchoukina, Olga Viktorovna and C{\^a}ndido, Pedro 
                         Ant{\^o}nio and Costa, Rafael Lopes and Rodrigues, Marcelo 
                         Petry",
          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)} and {Instituto Nacional de 
                         Pesquisas Espaciais (INPE)}",
                title = "TUCA heat pipes experiment",
            booktitle = "Proceedings...",
                 year = "2014",
         organization = "International Conference Heat Pipes for Space Applications, 2.",
             keywords = "Heat Pipe.",
             abstract = "A heat pipe (HP) experiment named TUCA (acronyms for {"}Tubo de 
                         Calor{"}, in Portu-guese), to be probably flown on ITASAT 
                         University satellite is proposed. The experiment consists of an 
                         axially-grooved aluminum acetone-charged heat pipe positioned at 
                         the center of a spin-stabilized satellite along its spin axis. Two 
                         L-shaped saddles provide thermal cou-pling with the top and bottom 
                         satellite panels; the temperature difference between these two 
                         panels yields necessary driving gradient temperature for the HP 
                         operating. Special metallic plates at the HP interfaces (doublers) 
                         provide the HP input-output heat rates. High precision thermistors 
                         installed along the HP length allow the detection of any 
                         Non-Condensable Gases (NCG) blockage expansion. A developed 
                         SINDA/FLUINT Thermal Desktop® TUCA ther-mal model is used to 
                         predict the HP behavior under flight conditions and for 
                         elaboration of thermal vacuum tests specification.",
  conference-location = "Moscow",
      conference-year = "2014",
                label = "lattes: 1120380722483382 3 SantosBGBMKCCR:2014:TUHePi",
             language = "en",
           targetfile = "Santos_TUCA.pdf",
        urlaccessdate = "28 mar. 2024"
}


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