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
โฆ LIBER โฆ
Design of a thermal system for thermovacuum chambers
โ Scribed by M. Thirumaleshwar
- Publisher
- Elsevier Science
- Year
- 1978
- Tongue
- English
- Weight
- 547 KB
- Volume
- 18
- Category
- Article
- ISSN
- 0011-2275
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