Universal Responses of Cyclic-Oxidation Models Studied
Alloy Design Workbench--Surface Modeling Package Developed
Ballistic Impact Response of Advanced Silicide Alloys Tested in the IHPTET Program
Versatile Turbine Disk Alloy Designed and Processed for Higher Temperature Applications
Superalloy Disk With a Dual Grain Structure Spin Tested
High-Temperature Oxidation-Resistant and Low Coefficient of Thermal Expansion NiAl-Base Bond Coat Developed for Turbine Blade Application
Superior Ballistic Impact Performance Achieved by the Co-Base Alloy Haynes 25
Alloy Design Data Generated for B2-Ordered Compounds
Superalloy Lattice Block Developed for Use in Lightweight, High-Temperature Structures
Processing Methods Established To Fabricate Porous Oxide Ceramic Spheres for thermal Barrier Coating Applications
Creep Resistance of ZrO2 Ceramic Improved by the Addition of a Small Amount of Er2O3
Oxidation of Carbon Fibers in a Cracked Ceramic Matrix Composite Modeled as a Function of Temperature
Cooled Ceramic Composite Panel Successfully Tested in Rocket Combustion Facility
Uncooled C/SiC Composite Chamber Tested Successfully in Rocket Combustion Lab
Ultra-High-Temperature Ceramics Evaluated for Aeropropulsion Use
Polymer/Silicate Nanocomposites Developed for Improved Strength and Thermal Stability
New Method Developed To Purify Single Wall Carbon Nanotubes for Aerospace Applications
High-Temperature Polymer Composites Studied for Space Propulsion Applications
Multiple Knudsen Cell Configuration Improved for Alloy Activity Studies
Studies Conducted on Sodium Carbonate Contaminant Found on the Wing Leading Edge and the Nose Cap of the Space Shuttle Orbiter
Advanced Environmental Barrier Coatings Developed for SiC/SiC Composites Vanes
Low Thermal Conductivity Thermal Barrier Coatings Developed
New Oxide Ceramic Developed for Superior High-Temperature Wear Resistance
NASA Glenn/AADC-Rolls Royce Collaborated to Measure Erosion Resistance on Coated Polymer Matrix Composites
Oxidation of Carbon Fibers in Water Vapor Studied
NiAl Coatings Investigated for Use in Reusable Launch Vehicles
Combustor and Vane Features and Components Tested in a Gas Turbine Environment
Last updated: June 25, 2003
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