System Level Impact of Landing Point Redesignation for High-Mass Mars Missions
Survey of Blunt Body Dynamic Stability in Supersonic Flow
Rapid Simultaneous Hypersonic Aerodynamic and Trajectory Optimization Using Variational Methods
Rapid Simultaneous Hypersonic Aerodynamic and Trajectory Optimization Using Variational Methods
Rapid Entry Corridor Trajectory Optimization for Conceptual Design
Rapid Design Space Exploration for Conceptual Design of Hypersonic Missions
Rapid Design Space Exploration for Conceptual Design of Hypersonic Missions
Oscillation of Supersonic Inflatable Aerodynamic Decelerators at Mars
High Mass Mars Entry, Descent, and Landing Architecture Assessment
Application of a Reynolds-Averaged Navier-Stokes Approach to Supersonic Retropropulsion Flowfields
AIAA-2006-6276 An Evaluation of Ballute Entry Systems for Lunar Return Missions
Aerodynamic and Aeroelastic Characteristics of a Tension Cone Inflatable Aerodynamic Decelerator
Aerodynamic and Aeroelastic Characteristics of a Tension Cone Inflatable Aerodynamic Decelerator
Aerodynamic Analysis of Next Generation Supersonic Decelerators (AIAA 2014-2990)