Report on the Fracture Analysis of HfB(sub 2)-SiC and ZrB(sub 2)-SiC Composites; TOPICAL
Description
Hafnium diboride-silicon carbide (HS) and zirconium diboride-silicon carbide (ZS) composites are potential materials for high temperature, thermal shock applications such as for components on re-entry vehicles. In order to establish material constants necessary for evaluation of in situ fracture, bars fractured in four-point flexure were examined using fractographic principles. The fracture toughness was determined from measurements of the critical crack sizes and the strength values and the crack branching constants were established to use in forensic fractography for future in-flight tests. The fracture toughnesses range from about 13 MPam(sup 1/2) at room temperature to about 6 MPam(sup 1/2) at 1400 C for ZrB(sub 2)-Sic composites and from about 13 MPam(sup 1/2) at room temperature to about 4 MPam(sup 1/2) at 1400 C for HfB(sub 2)-SiC composites. Thus, the toughnesses of either the HS or ZS composites have the potential for use in thermal shock applications. Processing and manufacturing defects limited the strength of the test bars. However, examination of the microstructure on the fracture surfaces shows that the processing of these composites can be improved. There is potential for high toughness composites with high strength to be used in thermal shock conditions if the processing and handling are controlled
Availability note (English)
Available from Sandia National Labs., Albuquerque, NM (US)Additional details
Publishing Information
- Imprint Pagination
- 41 p.
- Report number
- SAND--2001-2898
INIS
- Country of Publication
- United States
- Country of Input or Organization
- United States
- INIS RN
- 33068840
- Subject category
- S36: MATERIALS SCIENCE;
- Resource subtype / Literary indicator
- Non-conventional Literature
- Descriptors DEI
- COMPOSITE MATERIALS; DEFECTS; FRACTURE PROPERTIES; HAFNIUM BORIDES; MICROSTRUCTURE; REENTRY VEHICLES; SILICON CARBIDES; THERMAL SHOCK; ZIRCONIUM BORIDES
- Descriptors DEC
- BORIDES; BORON COMPOUNDS; CARBIDES; CARBON COMPOUNDS; HAFNIUM COMPOUNDS; MATERIALS; MECHANICAL PROPERTIES; REFRACTORY METAL COMPOUNDS; SILICON COMPOUNDS; SPACE VEHICLES; TRANSITION ELEMENT COMPOUNDS; VEHICLES; ZIRCONIUM COMPOUNDS
Optional Information
- Contract/Grant/Project number
- AC04-94AL85000
- Funding organization
- US Department of Energy (United States)