Multi-Node Modeling of Cryogenic Tank Pressurization System using Generalized Fluid System Simulation Program

Bandyopadhyay, Alak ; Majumdar, Alok K ; Leclair, Andre C ; Valenzuela, Juan G

关键词: FUEL TANK PRESSURIZATION;    CRYOGENIC TANKS;    PROPELLANT TANKS;    CRYOGENIC ROCKET PROPELLANTS;    ULLAGE;    SIMULATION;    LIQUID NITROGEN;    CONDUCTIVE HEAT TRANSFER;    AXIAL FLOW;   

RP-ID  :  M19-7513

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

This paper presents a multi-node model of autogenous pressurization of cryogenic propellant in a flight tank using the Generalized Fluid System Simulation Program (GFSSP), a general purpose flow network code developed at NASA/Marshall Space Flight Center. Tests were conducted to measure the pressure and temperatures at the various axial locations of the stratified ullage at 75% and 45% fill level. Liquid nitrogen was pressurized by gaseous nitrogen from a supply tank while the drain valve from the tank remained closed during the pressurization process. The ullage was discretized into 25 uniformly distributed nodes: 5 in the radial direction and 5 in the axial direction assuming the flow to be axisymmetric. Heat and mass transfer between the liquid and vapor has been modeled at the liquid vapor interface. Heat transfer between wall and vapor at the ullage has been accounted for by assuming heat transfer occurs by natural convection. The model also accounts for heat leak to the tank through the insulation and metal wall by heat conduction. The predicted pressures and temperatures are compared with the measured data.