NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Numerical Modeling of No Vent Filling of a Cryogenic Tank with Thermo-dynamic Vent System Assisted InjectorThis paper presents a multi-node finite volume model of No Vent Filling (NVF) of a cryogenic tank with Thermo-dynamic Vent System (TVS) assisted injector, using the Generalized Fluid System Simulation Program (GFSSP), a general purpose flow network code. NVF tests were conducted in a CRYOgenic Orbital Testbed (CRYOTE) tank which was filled by liquid nitrogen using a TVS assisted injector with vent valve closed during the entire filling process. In TVS assisted injector, the liquid flow splits into two streams: one stream is routed to a Joule-Thomson (J-T) orifice where the flow immediately flashes from liquid to vapor or two phase mixture because the downstream to J-T leg is maintained at vacuum level.; the other stream is injected into the tank after being cooled by cold vapor of J-T leg in a heat exchanger. The flow through J-T leg is also used to cool the outer metal matrix of the injector which in turn cools the vapor in the tank ullage. The cooling of vapor in the ullage by cold injector surface reduces ullage pressure that allows liquid to enter and fill the tank. An integrated numerical model of the test set up was developed. The model included the dual lines of TVS assisted injector, tank and tank wall. 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 at ullage-injector interface and when it comes in contact with the liquid spray. The predicted pressure, resident mass, wall temperature in the tank were compared with the test data.
Document ID
20210023960
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
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)
Mostafa Ghiaasiaan
(Georgia Institute of Technology Atlanta, Georgia, United States)
Date Acquired
November 4, 2021
Subject Category
Fluid Mechanics And Thermodynamics
Meeting Information
Meeting: 29th Space Cryogenics Workshop
Location: Virtual
Country: US
Start Date: November 15, 2021
End Date: November 16, 2021
Sponsors: Cryogenics Society of America
Funding Number(s)
WBS: 012873.05.02.01,62
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available