| タイトル | Permeability of Impacted Coated Composite Laminates |
| 本文（外部サイト） | http://hdl.handle.net/2060/20020070788 |
| 著者（英） | Johnson, W. S.; Findley, Benjamin |
| 著者所属（英） | Georgia Inst. of Tech. |
| 発行日 | 2002-08-01 |
| 言語 | eng |
| 内容記述 | Composite materials are being considered for use on future generations of Reusable Launch Vehicles (RLVs) for both fuel tanks and fuel feedlines. Through the use of composite materials NASA can reduce the overall weight of the vehicle dramatically. This weight savings can then be translated into an increase in the weight of payload sent into orbit, reducing the cost per pound of payload. It is estimated that by switching to composite materials for fuel tanks the weight of the tanks can be reduced by 40 percent, which translates to a total vehicle weight savings of 14 percent. In this research, carbon/epoxy composites were studied for fuel feedline applications. There are concerns about using composite materials for feedlines and fuel tanks because these materials are extremely vulnerable to impact in the form of inadvertent bumping or dropped tools both during installation and maintenance. Additionally, it has been found that some of the sample feedlines constructed have had leaks, and thus there may be a need to seal preexisting leaks in the composite prior to usage. |
| NASA分類 | Composite Materials |
| レポートNO | E-18-675 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/91289 |
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