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Numerical Modeling of No Vent Filling of a Cryogenic TankThis paper presents a multi-node finite volume model of the chilling and filling of a cryogenic tank using the Generalized Fluid System Simulation Program (GFSSP), a general purpose flow network code. Vented Chill and No Vent Fill (VCNVF) tests were conducted at Marshall Space Flight Center where a flight-like tank was filled with liquid nitrogen from a supply tank. In the VCNVF tests, the tank was partially chilled while the vent valve was open. After the partial chilling, the vent valve was closed and the tank was filled without any venting. An integrated numerical model of the test set up was developed. The model included the transfer line from the supply tank, the target tank with the spray nozzle and solid walls, and the discharge line with the vent valve. The tank was discretized into multiple fluid nodes and branches to represent the ullage and liquid nitrogen and multiple solid nodes to represent the tank wall and structure. The heat transfer between solid to fluid was calculated from pool boiling correlations which include film, transition, and nucleate boiling, as well as natural convection during pre- and post-boiling. The model also accounts for the condensation of vapor in the tank when it comes in contact with the liquid spray. The predicted pressure, resident mass, wall and ullage temperature in the tank were compared with the test data.
Document ID
20205004529
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Alok Majumdar
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Andre LeClair
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Jason Hartwig
(Glenn Research Center Cleveland, Ohio, United States)
Adam Martin
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Noah Rhys
(Jacobs (United States) Dallas, Texas, United States)
Date Acquired
July 16, 2020
Subject Category
Propellants And Fuels
Meeting Information
Meeting: AIAA Propulsion and Energy Forum
Location: Online
Country: US
Start Date: August 24, 2020
End Date: August 26, 2020
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 80MSFC18C0011
Distribution Limits
Public
Copyright
Public Use Permitted.
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