| タイトル | Development of a special purpose spacecraft interior coating, phase 3 |
| 本文（外部サイト） | http://hdl.handle.net/2060/19800006940 |
| 著者（英） | Gillman, H. D.; Nannelli, P. |
| 著者所属（英） | Pennwalt Corp. |
| 発行日 | 1979-04-01 |
| 言語 | eng |
| 内容記述 | 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. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 80N15199
NASA-CR-160441 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/173688 |
