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
Part-Task Simulator for Truck Transmission Gear Shifting
Post-Flight Testing and Analysis of Zero-G Foam Rigidized Struts
AIAA-2006-1805 Measurement of In-Plane Motion of Thin-Film Structures Using Videogrammetry
Staged Microgravity Deployment of a Pressurizing Scale Model Spacecraft
Design and Flight Testing of Inflatable Wings with Wing Warping
Aeroelastic Behavior of Inflatable Wings: Wind Tunnel and Flight Testing AIAA Paper
Effect of Real and Simulated Space Flight on Collagen Crosslink Excretion
Flight Control of a UAV with Inflatable Wings with Wing Warping
AIAA-2006-1697 Development of a Finite Element Model of Warping Inflatable Wings
Experimental Analysis of Carbon Nitridation and Oxidation Efficiency with Laser-Induced Fluorescence
AIAA-2004-6570 Flying on Air: UAV Flight Testing with Inflatable Wing Technology
Stowed Unmanned Air Vehicle Engineering (SUAVE): Deployable Wing Design and Testing
Flight Testing and Simulation of a Mars Aircraft Design Using Inflatable Wings AIAA Paper
Experimental Results Regarding Two-Dimensional Deployment of Inflatable Beams
AIAA-2001-1264 Experimental Results Regarding the Inflation of Unfolding Cylindrical Tubes
Testing of Compact Inflatable Wings for Small Autonomous Aircraft
Development and Flight Testing of a UAV with Inflatable-Rigidizable Wings
Modeling and Characterization of Damage Processes in Metallic Materials
Recent Results on Liquid Fuelled APU for Truck Application
AIAA-2006-1696 A High-Altitude Test of Inflatable Wings for Low-Density Flight Applications
A Reusable Space Vehicle Design Study Exploring Sharp Leading Edges
Low Speed Aerodynamics and Landing Characteristics of Sharp-Class Crew Transfer Vehicle Concepts
A Preliminary Evaluation of Child Restraints and Anchorage Systems for an Australian Car
2008-01-0777 Experimental Validation of a Coupled Fluid-Multibody Dynamics Model for Tanker Trucks
SPICE modeling of ferroelectric liquid crystal on silicon microdisplays [5181-21]
A Pressurized Deployment Model for Inflatable Space Structures