Rapid Design Space Exploration for Conceptual Design of Hypersonic Missions
Rapid Design Space Exploration for Conceptual Design of Hypersonic Missions
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
Application of a Reynolds-Averaged Navier-Stokes Approach to Supersonic Retropropulsion Flowfields
Survey of Blunt Body Dynamic Stability in Supersonic Flow
Oscillation of Supersonic Inflatable Aerodynamic Decelerators at Mars
System Level Impact of Landing Point Redesignation for High-Mass Mars Missions
Aerodynamic Analysis of Next Generation Supersonic Decelerators (AIAA 2014-2990)
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
High Mass Mars Entry, Descent, and Landing Architecture Assessment