Aerospace Mechanisms Symposium (21st)
Recent NASA Progress in Composites
Preliminary Design Approach for Large High Precision Segmented Reflectors
Rigid Mid-Lift-to-Drag Ratio Approach to Human Mars Entry, Descent, and Landing
Hypersonic Inflatable Aerodynamic Decelerator (HIAD) Technology Development Overview
Hypersonic Inflatable Aerodynamic Decelerator (HIAD) Technology Development Overview
Aerospace Vehicle Design, Spacecraft Section. Volume 2: Project Groups 6 Through 8
Vacuum Leakage Tests of a Simulated Lightweight Spacecraft Air Lock
Hatch Integration Testing of a NASA TransHab Derivative Woven Inflatable Module
Sensitivity of Space Shuttle Weight and Cost to Structure Subsystem Weights
Automatic Docking Maneuver and Attitude Control System
Application of Autonomous Spacecraft Power Control Technology to Terrestrial Microgrids
Emulating a Flexible Space Structure: Modeling