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Cryogenic Propellant Tank Self-Pressurization and Active Pressure ControlThis AIAA Short Course lecture will present an overview of different experiments and computational modeling work that has been done to examine different aspects of pressurization and pressure control of a Cryogenic propellant tank. The lecture will cover several large-scale ground-based liquid Hydrogen cryogenic self-pressurization experiments that were performed at NASA Glenn and NASA Marshall, LN2 Nitrogen autogenous pressurization experiments, pressure control experiments using both subcooled jet mixing and subcooled droplet injection, and experiments that examined pressure drops that occur during tank sloshing. Numerical modeling and simulations that were done in association to these experiments as part of a comprehensive model validation effort will also be presented and discussed. Finally, the results of two simulant fluid pressurization and pressure control microgravity investigations performed as part of the Tank Pressure Control Experiment (TCPE) and The Zero-Boil-Off Tank (ZBOT)Experiment will also be presented.
Document ID
20240001073
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Mohammad Kassemi
(Case Western Reserve University Cleveland, United States)
Date Acquired
January 24, 2024
Subject Category
Fluid Mechanics and Thermodynamics
Meeting Information
Meeting: AIAA Online Short Course: Cryogenic Fluid Management for Storage & Transfer of Liquid Propellants in Space
Location: Virtual
Country: US
Start Date: January 30, 2024
End Date: February 8, 2024
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 619352.06.11.03.04.01
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
Single Expert
Keywords
Propellant Management
Two-Phase-Flow
CFD Modelling
Phase Change
Microgravity Fluids and Heat Transfer
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