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Daniel Guggenheim School of Aerospace Engineering
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High Mass Mars Entry, Descent, and Landing Architecture Assessment
Experimental Determination of Material Properties for Inflatable Aeroshell Structures
Computational Aerodynamic Analysis of a Tension Cone Supersonic Inflatable Aerodynamic Decelerator
Multiobjective Hypersonic Entry Aeroshell Shape Optimization
Performance Characterization of Supersonic Retropropulsion for Application to High-Mass Mars Entry, Descent, and Landing
The State of Problem Decomposition in Engineering Design
Ablative Thermal Response Analysis Using the Finite Element Method
Aerodynamic and Aeroelastic Characteristics of a Tension Cone Inflatable Aerodynamic Decelerator
Trajectory Reconstruction of a Martian Planetary Probe Mission: Reconstruction of the Spirit Mars Exploration Rover Entry Descent Landing Performance