Organizational Unit:
Daniel Guggenheim School of Aerospace Engineering
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BioDOME: Concept of an EDL System for Returning Small Biological Samples from LEO
Conceptual Modeling of Supersonic Retropropulsion Flow Interactions and the Relationship to System Performance
Subsonic and Transonic Wind Tunnel Testing of Two Inflatable Aerodynamic Decelerators
Entry, Descent, and Landing System Design for the Mars Gravity Biosatellite
Integrated Trajectory, Atmosphere, and Aerothermal Reconstruction Methodology Using the MEDLI Dataset
Statistical Entry, Descent and Landing Performance Reconstruction of the Mars Phoenix Lander
Entry, Descent, and Landing System Design for the Mars Gravity Biosatellite
Mass Model Development for Conceptual Design of a Hypersonic Rigid Deployable Decelerator
Performance Characterization, Sensitivity and Comparison of a Dual Layer Thermal Protection System
Introducing PESST: A Conceptual Design and Analysis Tool for Unguided/Guided EDL Systems