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Full Scale Flat Floor Testing of a 500-M2-Class Solar Sail Deployer
Space Flight Requirements for Fiber Optic Components Qualification Testing and Lessons Learned
Advanced Carbon-Carbon Materials for Solid Rocket Nozzles
Automated Fiber Placement: Evolution and Current Demonstrations
Fiber-Optic Sensing System: Overview, Development and Deployment in Flight at NASA
Establishing a Disruptive New Capability for NASA to Fly UAV's into Hazardous Conditions
Use of Composite Materials for Helicopter Rotor Blades
Flexible Wing Designs with Sensor Control Feedback for Demonstration on the X-56A (MUTT)
Fiber Optic Collective Flight Control System for Helicopters
Spaceborne Fiber Optic Data Bus (SFODB)
Characterization of Subsystems for a WB-003 Single Stage Shuttle
Laser Ignition Technology for Bi-Propellant Rocket Engine Applications
Continuous Trailing-Edge Flaps for Primary Flight Control of a Helicopter Main Rotor
Advanced Fiber Optic-Based Sensing Technology for Unmanned Aircraft Systems
Partnership Opportunities with AFRC for Wireless Systems Flight Testing
Design, Fabrication and Laboratory Testing of a Helicopter Composite Main Rotor Hub
Development of Energy Dissipating Plastic Honeycomb Quarterly Progress Report, 1 Aug. - 31 Oct. 1966
The Development of Low Elastic Webbings for Use in the Fabrication of Restraint Harnesses
Flight-Testing of the FAA Onboard Inert Gas Generation System on an Airbus A320
Conceptual Design of an Inertial Navigation System for an Autonomous Submersible Testbed Vehicle
Conceptual Design of Navy Composite Wings
Airborne-Fiber Optics Manufacturing Technology, Aircraft Installation Processes