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
BioDOME: Concept of an EDL System for Returning Small Biological Samples from LEO
Conceptual Modeling of Supersonic Retropropulsion Flow Interactions and the Relationship to System Performance
Subsonic and Transonic Wind Tunnel Testing of Two Inflatable Aerodynamic Decelerators
A Survey of Ballute Technology for Aerocapture
Integrated Trajectory, Atmosphere, and Aerothermal Reconstruction Methodology Using the MEDLI Dataset
Statistical Entry, Descent and Landing Performance Reconstruction of the Mars Phoenix Lander
Entry, Descent, and Landing System Design for the Mars Gravity Biosatellite
Mass Model Development for Conceptual Design of a Hypersonic Rigid Deployable Decelerator
Performance Characterization, Sensitivity and Comparison of a Dual Layer Thermal Protection System
Evaluation of the Mars Pathfinder Parachute Drag Coefficient