Overview of the NASA Advanced Composite Solar Sail (ACS3) Technology Demonstration Project
Global Forum on Longevity of Structures
Structural Design Considerations for a 50 kW-Class Solar Array for NASA's Asteroid Redirect Mission
Loads and Sizing for Launch Vehicle Conceptual and Preliminary Design
ACS3 – A 12U Solar Sail Technology Demonstration
Role of Structural Models in the Solar Sail Flight Validation Process
Zero-G Experiments of the BionicWingsat - A 2U-Cubesat with Deployable, Biologically-Inspired Wings
Space Shuttle Stiffener Ring Foam Failure Analysis, A Non-Conventional Approach
Space Assembly of Large Structural System Architectures (SALSSA)
BILL-E: Robotic Platform for Locomotion and Manipulation of Lightweight Space Structures
Space structures technology for future flight systems
Delayed Simultaneous Release Mechanism Patent Application
Spacelab Soft Mockup Comparative Evaluation
Design-Development Testing - Space Vehicle Design Criteria
Computation of Structural Modes of a Rollout Array Spacecraft for Attitude Control Study
Advanced Structures: 2000-2004
Applications of Structural Optimization Methods to Fixed-Wing Aircraft and Spacecraft in the 1980s
Shourai No Uchuuki Shisutemu No Kenkyuu (Research on Advanced Spacecraft)
Staging Loads - Space Vehicle Design Criteria
Spacecraft 2000: The Challenge of the Future
Preliminary Design Method for Deployable Spacecraft BEAMS
Optimization of a Multifunctional Hot Structure Aeroshell for Mars Entry
Baseline Tests of an Autonomous Telerobotic System for Assembly of Space Truss Structures
Planetary Explorer Structural Concept Evaluation Model Using Nastran
Construction and Control of Large Space Structures
Lightweight Multifunctional Planetary Probe for Extreme Environment Exploration and Locomotion
Bigelow Expandable Activity Module (BEAM) Monitoring System
In-Space Manufacturing: Pioneering a Sustainable Path to Mars
Toward Radiation-Smart Structures and Designs
Aerospace Vehicle Design, Spacecraft Section. Volume 1: Project Groups 3 Through 5
Preliminary Design Approach for Large High Precision Segmented Reflectors
Design Study of an Integrated Aerobraking Orbital Transfer Vehicle
Space Tug Systems Study (Storable). Volume 3: Executive Summary
Aerospace Mechanisms Symposium (21st)
Recent NASA Progress in Composites
Aerospace Vehicle Design, Spacecraft Section. Volume 2: Project Groups 6 Through 8
Vacuum Leakage Tests of a Simulated Lightweight Spacecraft Air Lock
Sensitivity of Space Shuttle Weight and Cost to Structure Subsystem Weights