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Thermal properties UHTC composites

Ceramic borides, carbides and nitrides are characterized by high melting points, chemical inertness and relatively good oxidation resistance in extreme environments, such as conditions experienced during reentry. This family of ceramic materials has come to be known as Ultra High Temperature Ceramics (UHTCs). Some of the earliest work on UHTCs was conducted by the Air Force in the 1960 s and 1970 s. Since then, work has continued sporadically and has primarily been funded by NASA, the Navy and the Air Force. This article summarizes some of the early works, with a focus on hafnium diboride and zirconium diboride-based compositions. These works focused on identifying additives, such as SiC, to improve mechanical or thermal properties, and/or to improve oxidation resistance in extreme environments at temperatures greater than 2000°C. [Pg.197]

To achieve fracture in UHTC materials, ManLabs researchers decided to notch all subsequent test specimens. Notches were 6 mm deep x 1.6 mm wide and parallel to the axis of the cylinder, extending inward from the outer surface along the entire length of the specimen. The main disadvantage of using notched specimens was the lack of adequate experimental and analytical data on the shape factor required to compare the experimental results with predicted properties as well as the inability to compare these results with those of previous evaluations. Their results showed that materials with SiC and carbon additions displayed somewhat higher steady state thermal stress resistance than the other compositions. Nonetheless, all the diboride compositions tested showed a level of thermal stress resistance considerably above any other ceramics they had tested. ... [Pg.220]

UHTCs such as ZrB, HfB, and ZrC and their composites have been extensively investigated in recent years because of their excellent high temperature stiffness, high hardness, high thermal shock resistance, as well as the good oxidation and ablation resistance. These properties are essential for use as cladding materials in re-entry and ultra-high speed aircrafts to provide thermal protection under extreme environments. [Pg.655]


See other pages where Thermal properties UHTC composites is mentioned: [Pg.297]    [Pg.198]    [Pg.72]    [Pg.81]    [Pg.279]    [Pg.355]    [Pg.429]   


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