Ventless pressure control of two-phase propellant tanks in microgravity.
This work studies pressurization and pressure control of a large liquid hydrogen storage tank. A finite element model is developed that couples a lumped thermodynamic formulation for the vapor region with a complete solution of the Navier-Stokes and energy equations for the flow and temperature fields in the liquid. Numerical results show that buoyancy effects are strong, even in microgravity, and can reposition a vapor bubble that is initially at the center of the tank to a region near the tank wall in a relatively short time. Long-term tank pressurization with the vapor bubble at the tank wall shows that after an initial transient lasting about a week, the final rate of pressure increase agrees with a purely thermodynamic analysis of the entire tank. However, the final pressure levels are quite different from thermodynamic predictions. Numerical results also show that there is significant thermal stratification in the liquid due to the effects of natural convection. A subcooled jet is used to provide simultaneous cooling and mixing in order to bring the tank pressure back down to its initial value. Three different jet speeds are examined. Although the lowest jet speed is ineffective at controlling the pressure because of insufficient penetration into the liquid region, the highest jet speed is shown to be quite effective at disrupting thermal stratification and reducing the tank pressure in reasonable time.
Kassemi
Mohammad
M
National Center for Microgravity Research, NASA Glenn Research Center, 21000 Brookpark Road, MS110-3, Cleveland, OH 44135, USA. mohammad.kassemi@grc.nasa.gov
Panzarella
Charles H
CH
D006358:Hot Temperature; D006859:Hydrogen; D008962:Models, Theoretical; D011312:Pressure; D012212:Rheology; D018531:Spacecraft; D013696:Temperature; D013816:Thermodynamics; D014893:Weightlessness
D006859:Hydrogen