Modeling and Experimental Validation for the passive Thermodynamic Vent System (TVS) of cryogenic propellant tank

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Publisher
International Astronautical Federation (IAF)
Issue Date
2017-09-28
Language
English
Citation

68th International Astronautical Congress (IAC)

URI
http://hdl.handle.net/10203/227098
Appears in Collection
ME-Conference Papers(학술회의논문)
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