Strategic Objectives
• Master the chemical stability of non-ablative ceramic matrix composites.
• Understand the mechanics of crack deflection and fracture toughness.
• Explore the synthesis of silicon carbide and oxide-based fibers.
• Evaluate real-world performance under extreme thermal-structural loads.
The Core Challenge
Traditional aerospace materials fail at the sustained 2000°C temperatures required for next-generation hypersonic and space exploration hardware.
01
The Thermodynamics of Extremes
02
Ceramic Matrix Composites (CMC)
03
Beyond Ablation
04
The Chemistry of Silicon Carbide
05
Fiber Reinforcement Strategies
06
Chemical Vapor Infiltration
07
Oxidation and Corrosion
08
Ultra-High Temperature Ceramics
09
Fracture Mechanics
10
Pyrolysis and Precursors
11
Thermal Conductivity Management
12
Interface Coating Science
13
Carbon-Carbon Composites
14
Environmental Barrier Coatings
15
The Sintering Process
16
Non-Destructive Evaluation
17
Thermal Expansion Matching
18
Creep and Fatigue
19
Hypersonic Leading Edges
20
Plasma Testing Environments
21