| タイトル | Cyanate Ester and Phthalonitrile Impregnated Carbon Ablative TPS |
| 本文（外部サイト） | http://hdl.handle.net/2060/20160001148 |
| 著者（英） | Gasch, Matt; Boghozian, Tane; Stackpoole, Margaret M. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 2016-01-25 |
| 言語 | eng |
| 内容記述 | Phenolic resin has extensive heritage as a TPS (Thermal Protection Systems) material, however, alternative resin systems such as Cyanate Ester and Phthalonitrile may offer improved performance compared to state-of-the-art phenolic resin. These alternative resin systems may have higher char yield, higher char strength, lower thermal conductivity and improved mechanical properties. In current work at NASA Ames alternative resin systems were uniformly infused into fibrous substrates and preliminary properties characterized. The density of the cyanate ester infused in fibrous substrate ranged from 0.25-0.3 grams per cubic centimeter compared to PICA (Phenolic resin impregnated carbon ablative) having a density of approximately 0.25 grams per cubic centimeter. The density of Phthalonitrile varies from 0.22-0.25 grams per cubic centimeter. Initial formulations of these new resin systems were recently tested at the LARC HyMETs (Hypersonic Materials Environmental Test System) facility to evaluate their performance and data such as back face temperature, char yield, and recession are compared to PICA. Cyanate Ester and Phthalonitrile impregnated carbon ablative samples showed comparable performance to phenolic resin impregnated carbon ablative samples. |
| NASA分類 | Spacecraft Design, Testing and Performance; Fluid Mechanics and Thermodynamics; Composite Materials |
| レポートNO | ARC-E-DAA-TN26939 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
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