Development of a Novel Low Stored Volume High-Altitude Wing Design
Design Limitations of Deployable Wings for Small Low Altitude UAVS
Design Limitations of Deployable Wings for Small Low Altitude UAVs
High-Altitude LTA Airship Efforts at the U.S. Army SMDC/ARSTRAT
Altitude Comparison Technique Using the MC-130H APN-232 RADAR Altimeter
Testing of Compact Inflatable Wings for Small Autonomous Aircraft
2008-01-0777 Experimental Validation of a Coupled Fluid-Multibody Dynamics Model for Tanker Trucks
A New Model to Improve Aggregate Air Traffic Demand Predictions AIAA Paper
Challenges of Modeling Inflatable Wings AIAA Paper 2007-1848 CD-ROM Number 7
Aeroelastic Behavior of Inflatable Wings: Wind Tunnel and Flight Testing AIAA Paper
Landing Gear Mass Prediction - A Combined Analytic and Parametric Approach
ELECTRICAL ARC IGNITION TESTING OF SPACESUIT MATERIALS
Flight Testing and Simulation of a Mars Aircraft Design Using Inflatable Wings AIAA Paper