Fluid handling in spacecrafts  

Content: Subsystems of spacecraft Orbital mechanics Propulsion systems Mission design Governing equations Two-dimensional analysis of liquid/gas interface Dynamic behavior of liquids Liquid sloshing in closed containers Task of propellant management systems Basics of capillary rise Capillary rise in porous media Screen resistance and bubble point Design of propellant management components Outcome: Learning outcomes: Understanding the connection between accelerations of a spacecraft and liquid behavior Connection between thrust, acceleration, and propellant demand Understanding fluid mechanics on tank scale, component scale, and subcomponent scale Design tools for two-dimensional situations Design equations for propellant management devices
Presential
English
Fluid handling in spacecrafts
English

Funded by the European Union. Views and opinions expressed are however those of the author(s) only and do not necessarily reflect those of the European Union or HaDEA. Neither the European Union nor the granting authority can be held responsible for them. The statements made herein do not necessarily have the consent or agreement of the ASTRAIOS Consortium. These represent the opinion and findings of the author(s).