Core Material Families
Carbon-Carbon & SiC/SiC CMCs
Ultra-high temperature structural ceramics and carbon-fiber reinforced composites designed for turbine exhaust nozzles, leading edges, and re-entry vehicle thermal shielding.
Ti-6Al-4V ELI & Beta-C
Grade 5 titanium variants with enhanced fracture toughness and fatigue resistance. Optimized for cryogenic fuel tanks, landing gear, and high-cycle propulsion components.
CoCrFeMnNi & Refractory HEAs
Multi-principal element alloys exhibiting exceptional radiation tolerance, thermal stability, and mechanical strength under extreme cyclic loading conditions.
Aerogel Matrices & MLI Foils
Multi-layer insulation systems and silica-based aerogels providing passive thermal regulation for spacecraft buses, cryogenic pipelines, and payload fairings.
Testing & Characterization Facilities
Our materials division operates a closed-loop R&D ecosystem integrating computational design, rapid prototyping, and accelerated life testing. All facilities maintain ITAR-compliant secure environments.
Thermal Vacuum Chamber
±0.1K stability | 10⁻⁶ Torr | Simulated LEO/MEO cycles
Electron & X-Ray Diffraction
In-situ phase transformation mapping & defect analysis
SEM/TEM Microscopy
Atomic-scale grain boundary & composite interface imaging
Hypersonic Wind Tunnel
Mach 5–8 | Arc-heated | Ablation & heat flux measurement
Performance Specifications (Representative)
| Property | AeroVance CMC-7X | AeroVance Ti-BetaC | ASTM / AMS Ref |
|---|---|---|---|
| Tensile Strength (RT) | 420 MPa | 1150 MPa | ASTM E8 / AMS 4928 |
| Yield Strength (0.2% Offset) | 380 MPa | 980 MPa | ASTM E8 / AMS 4928 |
| Elongation at Break | 1.2% | 14.5% | ASTM E8 |
| Fatigue Limit (10⁷ cycles) | 210 MPa | 520 MPa | ASTM E466 |
| Thermal Conductivity | 18 W/m·K | 7.2 W/m·K | ASTM E1530 |
| Operating Temperature Range | -196°C to 1650°C | -253°C to 400°C | Internal Validation |
Key Aerospace Applications
Hypersonic Leading Edges
CMC and ultra-high temperature ceramic coatings resisting aerodynamic heating up to Mach 12 flight regimes.
Cryogenic Propellant Tanks
Aluminum-lithium and titanium alloy structures with internal MLI aerogel integration for LOX/LH2 storage.
Gas Turbine Hot Section
Single-crystal superalloys and thermal barrier coatings for high-pressure turbine blades and combustor liners.
Spacecraft Structural Frames
Carbon-fiber reinforced polymer (CFRP) and graphite-epoxy layups optimized for low thermal expansion and high stiffness-to-weight.
Research Partnerships & Publications
AeroVance's Materials Science division maintains active joint development agreements with NASA Glenn Research Center, DARPA's Materials Genome Initiative, and the European Space Agency's Advanced Materials Program. Peer-reviewed findings are published annually through the AeroVance Technical Journal (AVTJ) and presented at AIAA SciTech, MRS Spring, and the International Conference on Composite Materials.