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Daniel Guggenheim School of Aerospace Engineering
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Comparative Reliability of GEO, LEO, and MEO Satellites
High Mass Mars Entry, Descent, and Landing Architecture Assessment
Angle of Attack Modulation for Mars Entry Terminal State Optimization
Test Plan for the Technology Maturation of Supersonic Inflatable Aerodynamic Decelerators
Statistical Reliability Analysis of Satellites by Mass Category: Does Spacecraft Size Matter?
GT-FAST: A Point Design Tool for Rapid Fractionated Spacecraft Sizing and Synthesis
Performance Characterization of Supersonic Retropropulsion for Application to High-Mass Mars Entry, Descent, and Landing
Response Surface Equations for Expendable Launch Vehicle Payload Capability
Fast Sensitivity Computations for Trajectory Optimization
Trading Robustness Requirements in Mars Entry Trajectory Design