Slush-Hydrogen Technology
Report briefly describes some developments in technology of use of slush hydrogen as fuel in proposed National Aero-Space Plane (NASP).
Engineering topics
Publications and source records attributed to Tomsik, Thomas M..
Report briefly describes some developments in technology of use of slush hydrogen as fuel in proposed National Aero-Space Plane (NASP).
As part of the National Aero-Space Plane (NASP) project, the multi-dimensional effects of gravitational force, initial tank pressure, initial ullage temperature, and heat transfer rate on the 2-D temperature profiles were studied. FLOW-3D, a commercial finite difference fluid flow model, was used for the evaluation. These effects were examined on the basis of previous liquid hydrogen experimental data with gaseous hydrogen pressurant. FLOW-3D results were compared against an existing 1-D model. In addition, the effects of mesh size and convergence criteria on the analytical results were investigated. Suggestions for future modifications and uses of FLOW-3D for modeling of a NASP tank are also presented.