Organizational Unit:
Daniel Guggenheim School of Aerospace Engineering
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Structural impacts of inflatable aerodynamic decelerator design
Conceptual thermal response modeling, testing, and design of flexible heatshield insulation materials
Trajectory Trade-space Design for Robotic Entry at Titan
Supersonic Vehicle Configuration Transitions to Enable Supersonic Retropropulsion during Mars Entry, Descent, and Landing
Design and manufacturing of conformal ablative heatshields
Use of the Mars atmosphere to improve the performance of supersonic retropropulsion
Mechanical Design of a Cubesat Aeroshell for an Earth Demonstration of Single-Stage Drag Modulated Aerocapture
Magnetohydrodynamic energy generation and flow control for planetary entry vehicles
Development of an Earth SmallSat Flight Test to Demonstrate Viability of Mars Aerocapture
Mechanical property determination for flexible material systems