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The Life Prediction Branch features multiple world-class experimental research facilities designed to evaluate the full breadth of material behaviors under the extreme loading conditions and environments typical of aerospace propulsion applications. Materials of primary interest include monolithic ceramics and metallics, neat polymeric resins, and the multitude of fiber-reinforced composite forms generated when each is used as the matrix constituent.
In total, the Branch operates over fifty computer-controlled uniaxial and axial/torsion test frames designed to investigate a wide range of thermal, environmental and loading scenarios at the coupon and sub-component levels, including:
- Elastic properties (e.g., stiffness, Poisson's ratio, strength)
- Static deformation/failure (e.g., creep, stress relaxation)
- Quasi-static response (e.g., tension, compression, shear, bending)
- Low cycle and thermomechanical fatigue
- High cycle fatigue
- Long term fatigue/creep durability
- Fracture toughness
- Crack growth
Tests are conducted in a variety of environments including air, inert gases and vacuum, with temperature capabilities to 1650 degrees Celsius (3000 degrees Fahrenheit). Many unique facilities and specially designed testing apparatuses also exist to experimentally evaluate and characterize the advanced materials of interest.
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+ Learn more about available ceramics facilities
+ Learn more about available fatigue facilities
+ Learn more about available fracture facilities
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