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Transient thermal analysis of a cryogenic oxidizer tank in the liquid rocket propulsion system during the prelaunch helium gas pressurization

✍ Scribed by K. H. Kim; H. -J. Ko; K. Kim; Y. -S. Jung; S. -H. Oh; K. -J. Cho


Book ID
114994177
Publisher
SP MAIK Nauka/Interperiodica
Year
2012
Tongue
English
Weight
985 KB
Volume
21
Category
Article
ISSN
1810-2328

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