High Temperature Material Applications (HTMAS) Subcommittee
Technical Objectives
The principal objectives of the Subcommittee are:
- Promote communication among the federal government, rocket industry, materials producers, and related developers that support technology in high-temperature materials regarding design, analysis and modeling, testing and evaluation, processing science, and quality assurance.
- Recommend standard tools and procedures for design, analysis, and testing of high-temperature materials.
Scope
The scope of the High Temperature Material Applications Subcommittee includes promoting technical exchange and addressing problems associated with the use of advanced high-temperature materials, including carbon-carbon, ceramic-matrix, and carbon-phenolic composites, CERMETs, refractory metals, structural and non-structural insulators, and other advanced materials as applied to propulsion systems and related technology developments. Its areas of interest are design, development, analysis and modeling, testing and evaluation, processing science, and quality assurance, and applications include Rocket Nozzle Technology, Hypersonic Systems, Thrust Control, and components of Strategic, Tactical, Space Launch, and other systems.
Mission Areas
- Mission Area I: High Temperature Material Modeling and Simulation
- Mission Area II: High Temperature Material Design, Test and Evaluation
- Mission Area III: High Temperature Material Development
Click here for descriptions of each mission area.
JHU/WSE ERG Technical Representative
Ms. Claire Shamul, JHU WSE Energetics Research Group, Columbia, MD
Telephone:443-718-5011
Email:cshamul@erg.jhu.edu