Published By National Aeronautics and Space Administration
Issued over 9 years ago
Summary
Description
<p><strong>The project determined specific performance metrics and discrete technology development goals with which to gage proposed investments in ground propellant systems operations at SSC.&nbsp; Historical center studies/investigations were examined and surveyed on hydrogen and helium conservation and recovery. Additionally, a base analytic model of the Liquid Hydrogen (LH2) propellant tank at SSC&rsquo;s E1 test facility was developed and documented using Thermal Desktop</strong>&reg;/<strong>FlowCAD</strong>&reg;<strong>.</strong><strong> <em>FloCAD</em></strong>&reg;<strong> is a </strong><em>Thermal Desktop</em>&reg;<strong> module that allows a user to develop and integrate both fluid and </strong><em>thermal</em><strong> systems within a CAD based environment.</strong></p>