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