Organizational Unit:
Daniel Guggenheim School of Aerospace Engineering
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Entry, Descent, and Landing System Design for the Mars Gravity Biosatellite
Evaluation of the Mars Pathfinder Parachute Drag Coefficient
Introducing PESST: A Conceptual Design and Analysis Tool for Unguided/Guided EDL Systems
A Survey of Ballute Technology for Aerocapture
Entry, Descent, and Landing System Design for the Mars Gravity Biosatellite
Development of a Planetary Entry System Synthesis Tool for Conceptual Design and Analysis