Organizational Unit:
Daniel Guggenheim School of Aerospace Engineering
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Publication Search Results
Exploring the F6 Fractionated Spacecraft Trade Space with GT-FAST
Computational Fluid Dynamics Validation of a Single, Central Nozzle Supersonic Retropropulsion Configuration
Parametric Analysis and Targeting Capabilities for the Planetary Entry Systems Synthesis Tool
Initial Implementation of an Adjoint CFD Code for Aeroshell Shape Optimization
Analysis of Human-System Interaction For Landing Point Redesignation
Fully-Propulsive Mars Atmospheric Transit Strategies for High-Mass Missions
Guidance, Navigation, and Control Technology System Trades for Mars Pinpoint Landing
Experimental Determination of Material Properties for Inflatable Aeroshell Structures
Resonance Hopping Transfers Between Moon Science Orbits
Supersonic Retropropulsion Technology for Application to High Mass Mars Entry, Descent, and Landing