Aerospace Mechanisms Symposium (21st)
Preliminary Design Approach for Large High Precision Segmented Reflectors
Recent NASA Progress in Composites
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
Design Study of an Integrated Aerobraking Orbital Transfer Vehicle
Space Tug Systems Study (Storable). Volume 3: Executive Summary
Third Conference on Fibrous Composites in Flight Vehicle Design, Part 1
Conceptual Design and Evaluation of Selected Space Station Concepts, Volume 1
Development of Experimental/Analytical Concepts for Structural Design Verification
LDSD POST2 Modeling Enhancements in Support of SFDT-2 Flight Operations
Flight Performance of the Inflatable Reentry Vehicle Experiment 3
Numerical Simulation of the Inflation Process of Space Rigidized Antenna Structures
Effects of Variables Upon Pyrotechnically Induced Shock Response Spectra, Part 2
Examination of an Object from Space Undersoekning AV Rymdfragment
Design of Sert 2 Spacecraft Structures
Airborne Simulation of Launch Vehicle Dynamics
Active Control of Large Space Structures: An Introduction and Overview
Space Tug Systems Study. Volume 2: Compendium
Heisei 3 Nendo HOPE Gainen Sekkei (Concept Study of the Space Transportation System HOPE in FY 1991)
SCOLE (Spacecraft Control Laboratory Experiment) Design Challenge
33rd Aerospace Mechanisms Symposium
Temperature-Driven Shape Changes of the Near Earth Asteroid Scout Solar Sail
Space Station Redesign Option A: Modular Buildup Concept
Development of Inflatable Entry Systems Technologies
Plasma Interactions with Large Spacecraft
Impact of Vehicle Flexibility on IRVE-II Flight Dynamics
History of On-Orbit Satellite Fragmentations (14th Edition)
Habitability Study Shuttle Orbiter
Development of the Large Spacecraft Structure
Orion MPCV Service Module Avionics Ring Pallet Testing, Correlation, and Analysis