CS-063: Modelling of Spacecraft Propulsion System Priming in Flownex
This case study shows how Flownex was used as a tool to model a fuel feed system’s priming procedure, recording dynamic pressures during a transient simulation and investigating factors like fuel line friction, with experimental comparisons validating the model for future use.
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This case study highlights how Flownex was used to model the propellant feed system for the SAFFIRE rocket engine, determining tank pressure and flow characteristics, with results validated