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Air-cured ceramic coating insulates against high heat fluxes
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1965 |
| Description | Reflective insulating ceramic coating protects supporting structures in area adjacent to rocket engines from the intense heat fluxes in the rocket exhaust plumes. |
| File Size | 105937 |
| Page Count | 2 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19650000355 |
| Archival Resource Key | ark:/13960/t2j72610d |
| Language | English |
| Publisher Date | 1965-11-01 |
| Access Restriction | Open |
| Subject Keyword | Materials Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |