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Adhesive bonding of titanium to carbon-carbon composites for heat rejection systems
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Cerny, Jennifer Morscher, Gregory |
| Copyright Year | 2006 |
| Description | High temperature adhesives with good thermal conductivity, mechanical performance, and long term durability are crucial for the assembly of heat rejection system components for space exploration missions. In the present study, commercially available adhesives were used to bond high conductivity carbon-carbon composites to titanium sheets. Bonded pieces were also exposed to high (530 to 600 Kelvin for 24 hours) and low (liquid nitrogen 77K for 15 minutes) temperatures to evaluate the integrity of the bonds. Results of the microstructural characterization and tensile shear strengths of bonded specimens will be reported. The effect of titanium surface roughness on the interface microstructure will also be discussed. |
| File Size | 825933 |
| Page Count | 9 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20060051753 |
| Archival Resource Key | ark:/13960/t45q9wn2b |
| Language | English |
| Publisher Date | 2006-01-01 |
| Access Restriction | Open |
| Subject Keyword | Composite Materials Carbon-carbon Composites Metal Surfaces Microscopy Liquid Nitrogen Tensile Tests Mechanical Properties Titanium Thermal Conductivity Surface Roughness Adhesive Bonding Heat Radiators Microstructure Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
