Organizational Unit:
Space Systems Design Laboratory (SSDL)
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Publication Search Results
High Mass Mars Entry, Descent, and Landing Architecture Assessment
The State of Problem Decomposition in Engineering Design
Ablative Thermal Response Analysis Using the Finite Element Method
Design Space Pruning Heuristics and Global Optimization Method for Conceptual Design of Low-Thrust Asteroid Tour Missions
Performance Characterization of Supersonic Retropropulsion for Application to High-Mass Mars Entry, Descent, and Landing
Aerodynamic and Aeroelastic Characteristics of a Tension Cone Inflatable Aerodynamic Decelerator
Trajectory Reconstruction of a Martian Planetary Probe Mission: Reconstruction of the Spirit Mars Exploration Rover Entry Descent Landing Performance
Experimental Determination of Material Properties for Inflatable Aeroshell Structures
Computational Aerodynamic Analysis of a Tension Cone Supersonic Inflatable Aerodynamic Decelerator
Multiobjective Hypersonic Entry Aeroshell Shape Optimization