Aerospace high-temperature mechanical properties testing encompasses a suite of specialized analytical techniques designed to characterize the mechanical behavior of materials and components under elevated temperature conditions that simulate the extreme operational environments of aerospace systems. These environments include the sustained high temperatures (up to 1600°C and beyond) experienced by jet engine turbine blades, the cyclic thermal stress of spacecraft re-entry vehicles, and the combined high-heat and dynamic load conditions of hypersonic vehicle structures. Unlike ambient-temperature mechanical testing, this specialized field focuses on quantifying temperature-induced variations in material performance, including strength degradation, creep deformation, fatigue resistance, and fracture behavior, which directly govern the reliability and service life of aerospace materials. The core objective of such testing is to generate precise, reproducible data that supports the development of advanced materials—from nickel-based superalloys to ceramic matrix composites (CMCs)—by elucidating their performance limits under thermomechanical loading scenarios relevant to aerospace research.
Our Services
CD BioSustainable offers comprehensive, research-focused aerospace high-temperature mechanical properties testing services tailored to support the development of advanced materials for extreme environment applications. Our services are designed exclusively for the scientific research community, providing detailed characterization data that enables researchers to evaluate material performance, validate theoretical models, and optimize material formulations. Leveraging state-of-the-art testing infrastructure and decades of expertise in advanced materials characterization, we deliver precise, reproducible results that advance aerospace material research—from fundamental studies on microstructural evolution to applied research on component-level performance. Our team of materials scientists collaborates closely with clients to design customized testing protocols that address specific research objectives, ensuring that each test is aligned with the unique requirements of the material system and research question at hand.
Types of Our Services
High-Temperature Tensile and Compression Testing
Our high-temperature tensile and compression testing services quantify key mechanical parameters—including yield strength, ultimate tensile strength, elongation at break, and compressive modulus—across a temperature range of 25°C to 1500°C. Specimens are mounted in water-cooled grips to prevent thermal degradation of testing fixtures, and tests are conducted in controlled atmospheres (argon, nitrogen, or air) to simulate relevant environmental conditions. For example, we perform tensile testing on titanium alloy TA15 at 600°C to evaluate its suitability for compressor blade applications, measuring elongation at break and yield strength to assess structural integrity under sustained mid-temperature loading. This service also includes biaxial tensile testing for anisotropic materials like CMCs, which exhibit direction-dependent mechanical properties critical to their performance in aerospace structures.
Creep, Stress Rupture, and Fatigue Testing
We specialize in long-duration creep and stress rupture testing, which evaluates time-dependent deformation under constant high-temperature and stress conditions—essential for predicting the service life of engine components like turbine disks and combustor liners. Our testing systems maintain precise temperature control (±1°C) and load stability for durations up to 10,000 hours, generating creep curves that quantify primary, secondary, and tertiary creep phases. For thermomechanical fatigue testing, we simulate cyclic heating-cooling (from -50°C to 1200°C) combined with axial or torsional loading, replicating the operational cycles of aerospace components. We also conduct high-cycle fatigue (HCF) and low-cycle fatigue (LCF) testing at elevated temperatures, generating S-N curves that define fatigue life under varying stress amplitudes. A notable application of this service is the evaluation of TiAl intermetallic compounds for lightweight turbine components, where creep rate and fatigue life data inform material processing optimizations.
High-Temperature Fracture Mechanics and Thermal Shock Testing
Our fracture mechanics testing services quantify a material's resistance to crack propagation at elevated temperatures, including measurements of fracture toughness (KIC, JIC), fatigue crack growth rates (da/dN), and crack tip opening displacement (CTOD). These tests are critical for assessing the damage tolerance of materials like carbon-carbon composites used in hypersonic heat shields. We also offer thermal shock testing, which subjects materials to rapid temperature changes (up to 500°C/min) via water quenching or air cooling, simulating the thermal transients experienced during spacecraft re-entry or engine startup. For example, we evaluate the thermal shock resistance of yttria-stabilized zirconia (YSZ) thermal barrier coatings, measuring critical temperature differences and residual strength retention after multiple thermal cycles. This service includes post-test microstructural analysis via scanning electron microscopy (SEM) to characterize crack morphology and failure mechanisms.
Our Technologies
- High-Temperature Testing Systems and Heating Technologies
Our UTMs integrate specialized heating systems for aerospace materials:
- Resistance furnaces: Stable heating up to 1500°C (±2°C uniformity) for creep/tensile testing.
- Induction heating: Fast ramp rates (up to 500°C/min) for TMF testing, synchronized with mechanical loading.
- Plasma heating: Ultra-high temperatures (up to 2000°C) in inert atmospheres for refractory metals (Mo, W).
- All systems use Type R/S/B thermocouples and real-time temperature monitoring.
- Non-Contact Measurement and Data Acquisition Technologies
Non-contact techniques enable accurate high-temperature strain measurement:
- Laser extensometers: ±0.001% resolution up to 1800°C, no physical contact.
- DIC systems: Full-field strain mapping via high-speed cameras, detecting localized deformation and cracks.
- Data acquisition logs stress/strain/temperature/time at 1000 Hz, generating engineering curves and reports. Automated monitoring ensures data integrity for long-duration tests.
- Post-Test Analytical Techniques
Post-test analysis links microstructure to mechanical performance:
- SEM/EDS: Fracture surface analysis (dimples, cracks, oxides).
- XRD: Quantifies phase transformations (e.g., intermetallic precipitation in superalloys).
- DSC/TGA: Measures thermal stability and oxidation kinetics via mass/heat flow changes.
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