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Flexible thermal protection materials for entry systems
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Kourtides, Demetrius A. |
| Copyright Year | 1993 |
| Description | Current programs addressed in aeroassist flight experiment are: (1) evaluation of thermal performance of advanced rigid and flexible insulations and reflective coating; (2) investigation of lighter than baseline materials; (3) investigation of rigid insulations which perform well; (4) study of flexible insulations which require ceramic coating; and (5) study of reflective coating effective at greater than 15 percent. In National Aerospace Plane (NASP), the programs addressed are: (1) high and low temperature insulations; and (2) attachment/standoff methodology critical which affects thermal performance. |
| File Size | 165146 |
| Page Count | 10 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930012922 |
| Archival Resource Key | ark:/13960/t7zm0877f |
| Language | English |
| Publisher Date | 1993-02-01 |
| Access Restriction | Open |
| Subject Keyword | Space Transportation Spacecraft Reentry Flexible Bodies Thermal Protection Ceramic Coatings Temperature Effects Aeroassist Thermal Insulation Reentry Vehicles Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
