Organizational Unit:
Daniel Guggenheim School of Aerospace Engineering
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Publication Search Results
Mass Model Development for Conceptual Design of a Hypersonic Rigid Deployable Decelerator
Subsonic and Transonic Wind Tunnel Testing of Two Inflatable Aerodynamic Decelerators
Statistical Entry, Descent and Landing Performance Reconstruction of the Mars Phoenix Lander
Performance Characterization, Sensitivity and Comparison of a Dual Layer Thermal Protection System