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Development of a special purpose spacecraft interior coating, phase 3
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Gillman, H. D. Nannelli, P. |
| Copyright Year | 1979 |
| Description | A variety of intumescent coatings based on a fluorocarbon latex resin modified with either an acrylic resin or an epoxy resin were prepared. Several intumescent systems were used for these studies including some based on ammonium polyphosphate and others based on sulfanilamide. The best coatings developed had a high concentration (60-70% by wt.) of intumescent additives and had to be applied thick, approximately 100 mils, in order to have adequate intumescent/fire protection properties. |
| File Size | 1165004 |
| Page Count | 17 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19800006940 |
| Archival Resource Key | ark:/13960/t5k980g1b |
| Language | English |
| Publisher Date | 1979-04-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Design, Testing And Performance Sulfur Compounds Fire Prevention Aniline Ammonium Phosphates Epoxy Resins Acrylic Resins Human Factors Engineering Spacecraft Structures Fluorocarbons Protective Coatings 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 |
