Organizational Unit:
Space Systems Design Laboratory (SSDL)
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Publication Search Results
Methodology for Optimal Design of a Conformal Ablative Heatshield
Feasibility of Supersonic Retropropulsion Based on Assessment of Mars-Relevant Flight Data
Characterization of Guidance Algorithm Performance for Drag Modulation-Based Aerocapture
Thermogravimetric Analysis of Carbon Felt Insulation for Flexible Thermal Protection System Thermal Response Modeling
Mars Molniya Orbit Atmospheric Resource Mining
Advancing Supersonic Retropropulsion Using Mars-Relevant Flight Data: An Overview
Development of an Earth Smallsat Flight Test to Demonstrate Viability of Mars Aerocapture
Vacuum Infusion Process Development for Conformal Ablative Thermal Protection System Materials
Guidance Trades for High Ballistic Coefficient Mars Lander Trajectories
Design of a Novel Hypersonic Inflatable Aerodynamic Decelerator for Mars Entry, Descent, and Landing