PREPARATION OF THE KENTUCKY RE-ENTRY UNIVERSAL PAYLOAD SYSTEM FOR ORBITAL FLIGHT
Challenges of Modeling Inflatable Wings AIAA Paper 2007-1848 CD-ROM Number 7
Development of a Novel Low Stored Volume High-Altitude Wing Design
Effect of Boundary Conditions on Geometric Control for an Inflatable Pathfinder System
AIAA-2004-1503 Development of UV-Curable Inflatable Wings for Low-Density Flight Applications
Designing Collaborative Automated Planners for Agile Adaptation to Dynamic Change
BIG BLUE II: Mars Aircraft Prototype with Inflatable-Rigidizable Wings
Simulation of Deployment Dynamics of an Inflatable Solar Array
Design Limitations of Deployable Wings for Small Low Altitude UAVS
Design Limitations of Deployable Wings for Small Low Altitude UAVs
Altitude Comparison Technique Using the MC-130H APN-232 RADAR Altimeter