Cryogenic Propellant Tank Drain Simulation with a Stratified Ullage Nodal Model

Richard G Hibbs; Andre C LeClair; Alok K Majumdar

NASA NTRS · 20260004101

Cryogenic Propellant Tank Drain Simulation with a Stratified Ullage Nodal Model

Richard G Hibbs·Andre C LeClair·Alok K Majumdar

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Abstract

Cryogenic propellant tank pressurization systems maintain tank pressure within specified limits to comply with propellant thermodynamic and tank structural design requirements. Many pump-fed cryogenic liquid propulsion systems control tank pressure using an autogenous pressurization system. Autogenous pressurization systems vaporize and heat propellant to produce the pressurant gas delivered to the tank. While autogenous pressurization systems eliminate the need for a separate pressurant gas storage and delivery system, they couple pressurant mass requirements to propellant mass requirements. Accurate prediction of autogenous pressurant mass during propellant drain is essential in optimizing cryogenic propellant tank designs.

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BibTeX RIS

Richard G Hibbs, Andre C LeClair, Alok K Majumdar. Cryogenic Propellant Tank Drain Simulation with a Stratified Ullage Nodal Model. https://ntrs.nasa.gov/citations/20260004101

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