
UC Berkeley M.Eng. Capstone · Airbus U.S. Space & Defense
Liquid Xenon Propellant Slosh Dynamics
Capstone project with Airbus U.S. Space & Defense: a coupled CFD + 6DOF study quantifying how liquid Xenon slosh in a satellite propellant tank disturbs attitude, position, and torque — used to inform GNC design and slosh-mitigation trade studies.
My contribution
- Built Ansys Fluent CFD models of the Xenon tank to quantify disturbance forces across a range of acceleration profiles.
- Developed a Simulink 6DOF simulation coupling slosh forces into satellite attitude, position, and torque states.
- Identified worst-case operating conditions and characterized sensitivity of GNC performance to tank fill fraction.
- Presented findings to the cross-functional GNC team, enabling informed trade-offs on slosh feasibility and propellant energy reduction.
Documents & code

