Experimental and Computational Fluid Dynamics Study of Hayabusa Reentry Peak Heating
Design of Quasi-Terminator Orbits near Primitive Bodies
Parametric Study of Ballistic Lander Deployment to Small Bodies
In-flight Operation of the Dawn Ion Propulsion System Through Year One of Cruise to Ceres
Near-Infrared Spectroscopy of Hayabusa Sample Return Capsule Reentry
Spacecraft State Estimation Using Neural Radiance Fields
Trajectory Estimation of the Hayabusa Spacecraft During Atmospheric Disintegration