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Sharp Interface CFD Analysis of Noncondensable Gas Effects on 1G and Microgravity Tank Self-Pressurization and Pressure ControlIn future refueling depot and space operations, noncondensable gases (NCG)s may be used as pressurants to extract liquid propellant for tank-to-tank transfer and engine start-up operations. Once it is present in the ullage, the noncondensable gas can affect the interfacial evaporation and condensation processes that control tank self-pressurization and pressure control during subsequent storage. The Zero-Boil-Off-Tank-Noncondensable (ZBOT-NC) Experiment and its associated computational model development effort are carried out to study these phenomena. In this work, we present a Sharp Interface CFD (SI-CFD) model which is applied to the two-phase and two-component simulant fluid system used in the ZBOT-NC Experiment with Perfluoro-n-Pentane (PnP) as the simulant low-boiling point phase change fluid, and Xenon as the noncondensable gas. The SI-CFD model solves the continuity, momentum, energy, species, and turbulence equations in the vapor and liquid phases while providing very accurate temperature and species gradient calculations at the interface. In developing this model, particular attention was focused on the precise determination of the molar concentrations of the vapor and the noncondensable gas at the interface in order to correctly predict the vapor “Stefan wind” in the ullage, as well as the extent of the accumulation of the noncondensable gas at the phase front. Detailed microgravity and 1g numerical simulations and analyses are presented to show the characteristics of the noncondensable gas induced transport resistance in the ullage, along with the thermocapillary (Marangoni) convection in the liquid and their impact on the interfacial heat and mass transfer during tank self-pressurization and jet mixing pressure control. The results of these simulations indicate that, in 1g, the presence of the noncondensable gas affects pressure control noticeably but its impact on self-pressurization is minimal. However, in microgravity, the noncondensable gas seems to have a noticeable impact during self-pressurization while its effect on jet mixing pressure control is significant and considerably more pronounced than on earth.
Document ID
20250005911
Acquisition Source
Glenn Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Mohammad Kassemi
(Case Western Reserve University Cleveland, United States)
Sonya Hylton
(Case Western Reserve University Cleveland, United States)
Date Acquired
June 5, 2025
Publication Date
August 31, 2025
Publication Information
Publication: Cryogenics
Publisher: Elsevier
Volume:
Issue:
ISSN: 0011-2275
e-ISSN: 1879-2235
Subject Category
Fluid Mechanics and Thermodynamics
Spacecraft Propulsion and Power
Funding Number(s)
CONTRACT_GRANT: 80GRC020D0003
WBS: 448887.04.03.02
WBS: 619352.06.11.03.04.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
Keywords
TwoPhase Flow
Microgravity Fluids
Noncondensable Gases
Evaporation & Condensation
CFD
Propellant Tanks
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