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Microstructural investigation of high emittance glass coatings on fibrous ceramic insulation
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | DiFiore, Robert Ellerby, Don Loehman, Ron Figone, Jeff Kotula, Paul Leiser, Dan Smith, Dane |
| Copyright Year | 2001 |
| Description | This viewgraph presentation provides an overview of the Space Shuttle Thermal Protection System (TPS) and the various products incorporated in the TPS. There are three tile systems which include pure silica, fibrous refractory composite insulation (FRCI), and alumina enhanced thermal barrier (AETB). Coating systems include reaction cured glass (RCG) and toughened uni-piece insulation (TUFI). The microstructures of these systems are explored as are the manufacturing processes associated with each. Microstructural investigation using methods such as automated X-ray spectral image analysis (AXSIA) is a crucial part of understanding the mechanical nature of these systems. |
| File Size | 917504 |
| Page Count | 26 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20010095010 |
| Archival Resource Key | ark:/13960/t7xm3889p |
| Language | English |
| Publisher Date | 2001-01-01 |
| Access Restriction | Open |
| Subject Keyword | Nonmetallic Materials Insulation Thermal Protection Tiles Space Shuttles Glass Coatings Fiber Composites Ceramics X Ray Analysis Microstructure Silicon Dioxide Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |