Organizational Unit:
Daniel Guggenheim School of Aerospace Engineering
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Publication Search Results
Methodology for Optimal Design of a Conformal Ablative Heatshield
Advancing Supersonic Retropropulsion Using Mars-Relevant Flight Data: An Overview
Guidance Trades for High Ballistic Coefficient Mars Lander Trajectories
Design of a Novel Hypersonic Inflatable Aerodynamic Decelerator for Mars Entry, Descent, and Landing
Analytic Free-Molecular Aerodynamics for Rapid Propagation of Resident Space Objects
Mars Molniya Orbit Atmospheric Resource Mining
Characterization of Guidance Algorithm Performance for Drag Modulation-Based Aerocapture
Feasibility of Supersonic Retropropulsion Based on Assessment of Mars-Relevant Flight Data
Vacuum Infusion Process Development for Conformal Ablative Thermal Protection System Materials
Development of an Earth Smallsat Flight Test to Demonstrate Viability of Mars Aerocapture