Design aspects of the thermal system of
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M. Thirumaleshwar; M.R. Vyawahare; M. Pravin Kumar
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Article
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1982
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Elsevier Science
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English
โ 311 KB
Thermal system for a 4 m diameter x 4.5 m height thermovac chamber (TVC) designed for the Indian Space Research Organisation (ISRO) is described. Both the gaseous nitrogen (GN 2) and liquid nitrogen (LN 2) circulation systems are elaborated. Thermal analysis is shown in some detail. Design curves sh