Helium Pressurization Modeling of the EDU Submerged Diffuser Using Thermal Desktop

Hauser, Daniel

关键词: COMPUTATIONAL FLUID DYNAMICS;    CRYOGENIC ROCKET PROPELLANTS;    FLUID JETS;    FUEL TANK PRESSURIZATION;    HELIUM;    MICROGRAVITY;    PRESSURE REGULATORS;    CRYOGENIC FLUIDS;    EVAPORATION;    FLUID MANAGEMENT;    JET MIXING FLOW;    PREDICTION ANALYSIS TECHNIQUES;    REFUELING;   

RP-ID  :  GRC-E-DAA-TN60401

学科分类：力学，机械学

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

NASA is currently working on developing its predictive modeling capabilities to support future missions that require long term storage of cryogenic propellants. Through the Evolvable Cryogenics project, Development and Validation of Analysis Tools (DVAT) task, both CFD and multi-node fluid modeling tools are being validated against to increase the following cryogenic fluid management technologies: Self-Pressurization, Pressure Control, Helium Pressurization, de-stratification, jet mixing, Tank and transfer line chill-down, tank filling and transfer. NASA is using previous and future micro-gravity experiments to validate both types of models. Recent activities include: Validation of the Tank Pressure Control Experiment (TPCE), Hydrogen and Helium pressurization, and Completion of the Zero Boil Off Tank (ZBOT) experiment on ISS. Future activities include validation of the ZBOT experiment with both CFD and multi-node analysis tools, validation of the Cryogenic Demonstration System of the Robotic Refueling Mission (RRM3).