Organizational Unit:
Daniel Guggenheim School of Aerospace Engineering
Permanent Link
Research Organization Registry ID
Description
Previous Names
Parent Organization
Parent Organization
Includes Organization(s)
ArchiveSpace Name Record
Publication Search Results
Analysis of Human-System Interaction For Landing Point Redesignation
Fully-Propulsive Mars Atmospheric Transit Strategies for High-Mass Missions
Supersonic Retropropulsion Technology for Application to High Mass Mars Entry, Descent, and Landing
Low-Thrust Trajectory Optimization Tool to Assess Options for Near-Earth Asteroid Deflection
Experimental Determination of Material Properties for Inflatable Aeroshell Structures
Parametric Analysis and Targeting Capabilities for the Planetary Entry Systems Synthesis Tool
Initial Implementation of an Adjoint CFD Code for Aeroshell Shape Optimization
Computational Fluid Dynamics Validation of a Single, Central Nozzle Supersonic Retropropulsion Configuration
Guidance, Navigation, and Control Technology System Trades for Mars Pinpoint Landing
Smart Divert: A New Entry, Descent, and Landing Architecture