A NOVEL FMI AND TLM-BASED DESKTOP SIMULATOR FOR DETAILED STUDIES OF THERMAL PILOT COMFORT
Trajectory Options for Human Mars Missions AIAA Paper 2006-6308
Ablative Thermal Response Analysis Using the Finite Element Method
Multiobjective Hypersonic Entry Aeroshell Shape Optimization
AIAA-2005-2771 Daedalon: A Revolutionary Morphing Spacecraft Design for Planetary Exploration
Structural Verification and Modeling of a Tension Cone Inflatable Aerodynamic Decelerator
Oscillation of Supersonic Inflatable Aerodynamic Decelerators at Mars
Variable Angle-of-attack Profile Entry Guidance for a Crewed Lifting Body
Experimental Determination of Material Properties for Inflatable Aeroshell Structures
Experimental Determination of Material Properties for Inflatable Aeroshell Structures
AIAA-2004-6568 Flight System Options for a Long-Duration Mars Airplane
Entry, Descent and Landing Challenges of Human Mars Exploration (AAS 06-072)
AIAA-2006-6276 An Evaluation of Ballute Entry Systems for Lunar Return Missions
High Mass Mars Entry, Descent, and Landing Architecture Assessment
AIAA-2006-7427 Sizing of an Entry, Descent, and Landing System for Human Mars Exploration