| タイトル | Properties of Two Carbon Composite Materials Using LTM25 Epoxy Resin |
| 本文（外部サイト） | http://hdl.handle.net/2060/19970005119 |
| 著者（英） | Shah, C. H.; Cruz, Juan R.; Postyn, A. S. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1996-11-01 |
| 言語 | eng |
| 内容記述 | In this report, the properties of two carbon-epoxy prepreg materials are presented. The epoxy resin used in these two materials can yield lower manufacturing costs due to its low initial cure temperature, and the capability of being cured using vacuum pressure only. The two materials selected for this study are MR50/LTM25, and CFS003/LTM25 with Amoco T300 fiber; both prepregs are manufactured by The Advanced Composites Group. MR50/LTM25 is a unidirectional prepreg tape using Mitsubishi MR50 carbon fiber impregnated with LTM25 epoxy resin. CRS003/LTM25 is a 2 by 2 twill fabric using Amoco T300 fiber and impregnated with LTM25 epoxy resin. Among the properties presented in this report are strength, stiffness, bolt bearing, and damage tolerance. Many of these properties were obtained at three environmental conditions: cold temperature/dry (CTD), room temperature/dry (RTD), and elevated temperature/wet (ETW). A few properties were obtained at room temperature/wet (RTW), and elevated temperature/dry (ETD). The cold and elevated temperatures used for testing were -125 F and 180 F, respectively. In addition, several properties related to processing are presented. |
| NASA分類 | Structural Mechanics |
| レポートNO | 97N13087
NASA-TM-110286
NAS 1.15:110286 |
| 権利 | No Copyright |
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