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Nasa's Plans for Development of a Standard for Additively Manufactured Components
NASA International Environmental Partnerships
Status of Thermal NDT of Space Shuttle Materials at NASA
Lightweight Nonmetallic Thermal Protection Materials Technology
Technical Note: Some Issues Related to the Selection of Polymers for Aerospace Oxygen Systems
Analysis of a Preloaded Bolted Joint in a Ceramic Composite Combustor
High Temperature Polymeric Materials for Space Transportation Propulsion Applications
Thermal-Mechanical Cyclic Test of a Composite Cryogenic Tank for Reusable Launch Vehicles
Obtaining NASA Approval for use of Non-Metallic Materials in Manned Space Flight
Commercialization of NASA's High Strength Cast Aluminum Alloy for High Temperature Applications
Materials Science Work at NASA Ames Research Center
Analysis of Metallized Teflon(trademark) Film Materials Performance on Satellites
Preliminary Thermal-Mechanical Sizing of Metallic TPS: Process Development and Sensitivity Studies
Space Launch Initiative: New Capabilities - New Horizons
The Role of Ceramics and Ceramic Matrix Composites in NASA's Advanced Space Propulsion Programs
The Role of Ceramics and Ceramic Matrix Composites in NASA's Advanced Space Propulsion Programs
The Effect of Asymmetric Mechanical and Thermal Loading on Membrane Wrinkling
Flight Performance of a Functionally Gradient Material, TUFI, on Shuttle Orbiter
Preventing Spacecraft Failures Due to Tribological Problems
Composite Materials for Radiation Shielding During Deep Space Missions
Analysis of Ag/FEP Thermal Control Blanket Performance From Multiple Satellites
Metal Matrix Composite Materials for Aerospace Applications
Highlights of NASA's Role in Developing State-of-the-Art Nondestructive Evaluation for Composites
Aeroelastic Stability of A Soft-Inplane Gimballed Tiltrotor Model In Hover
Surface Characterization of LMMS Molybdenum Disilicide Coated HTP-8 Using Arc- Jet Hypersonic Flow
Novel Materials for Application as Shielding During Extended Space Flights
Marshall Convergent Coating Development Team: An Aerospace Success Story
Testing and Selection of Fire-Resistant Materials for Spacecraft Use
Pre-Launch Testing of GPS Receivers for Geodetic Space Missions
Development of the Spacecraft Materials Selector Expert System
Statistical Analysis of Strength Data for an Aerospace Aluminum Alloy
System Modelling of Rotary Ultrasonic Motors