Organizational Unit:
Daniel Guggenheim School of Aerospace Engineering
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Publication Search Results
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
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
Mars Molniya Orbit Atmospheric Resource Mining
Characterization of Guidance Algorithm Performance for Drag Modulation-Based Aerocapture
Thermogravimetric Analysis of Carbon Felt Insulation for Flexible Thermal Protection System Thermal Response Modeling