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Parametric Mass Modeling for Mars Entry, Descent and Landing System Analysis Study
PARAMETRIC MASS MODELING FOR MARS ENTRY, DESCENT AND LANDING SYSTEM ANALYSIS STUDY
OPTIMIZING MARS SPHERE OF INFLUENCE MANEUVERS FOR NASA'S EVOLVABLE MARS CAMPAIGN
Reusable launch vehicle engine systems operations analysis
Reusable Launch Vehicle Engine Systems Operations Analysis
Framework for the Parametric System Modeling of Space Exploration Architectures
Sustaining Human Presence on Mars Using ISRU and a Reusable Lander (AIAA 2015-4479)
Viability of a Reusable In-Space Transportation System (AIAA 2015-4580)
Optimization of the Mars Ascent Vehicle for Human Space Exploration