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Fiber
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Full Scale Flat Floor Testing of a 500-M2-Class Solar Sail Deployer
Application of high temperature composites to an aircraft component
Space Flight Requirements for Fiber Optic Components Qualification Testing and Lessons Learned
Advanced Carbon-Carbon Materials for Solid Rocket Nozzles
Rough handling tests of pacer and instapak foam-in-place of fuel tank assembly and pylon assembly
Angular weaving for turbine engine composite components
Automated Fiber Placement: Evolution and Current Demonstrations
Fiber-Optic Sensing System: Overview, Development and Deployment in Flight at NASA
Aussichten einer Anwendung des Diffusionsschweissens im Weltraum
Influence of constituent properties upon the structural efficiency of fibrous composite shell
Establishing a Disruptive New Capability for NASA to Fly UAV's into Hazardous Conditions
Use of Composite Materials for Helicopter Rotor Blades
Investigation of fiber systems of ablative materials Final report
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)
Experimental investigation of glass flakes as a liner for fiber-glass cryogenic propellant tanks
Improved cryogenic resin/glass-filament-wound composites Interim report, 29 Jun. 1965 - 28 Mar. 1966
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