Organizational Unit:
Space Systems Design Laboratory (SSDL)
Permanent Link
Research Organization Registry ID
Description
Previous Names
Parent Organization
Parent Organization
Includes Organization(s)
ArchiveSpace Name Record
Publication Search Results
Survey of Blunt Body Dynamic Stability in Supersonic Flow
Drag Modulation Flight Control for Aerocapture
Rapid Simultaneous Hypersonic Aerodynamic and Trajectory Optimization Using Variational Methods
Statistical Entry, Descent and Landing Performance Reconstruction of the Mars Phoenix Lander
Mass Model Development for Conceptual Design of a Hypersonic Rigid Deployable Decelerator
Comparison of Statistical Estimation Techniques for Mars Entry, Descent, and Landing Reconstruction from MEDLI-like Data Sources
Rapid Design Space Exploration for Conceptual Design of Hypersonic Missions
Guided Entry Performance of Low Ballistic Coefficient Vehicles at Mars
System Level Impact of Landing Point Redesignation for High-Mass Mars Missions
Performance Characterization, Sensitivity and Comparison of a Dual Layer Thermal Protection System
- «
- 1 (current)
- 2
- 3
- »