| タイトル | Fiberglass supports for cryogenic tanks |
| 本文（外部サイト） | http://hdl.handle.net/2060/19720025914 |
| 著者（英） | Keller, C. W. |
| 著者所属（英） | Lockheed Missiles and Space Co. |
| 発行日 | 1972-10-10 |
| 言語 | eng |
| 内容記述 | Analysis, design, fabrication, and test activities were conducted to develop additional technology needed for application of filament-wound fiberglass struts to cryogenic flight tankage. It was conclusively verified that monocoque cylinder or ogive struts are optimum or near-optimum for the range of lengths and loads studied, that a higher strength-to-weight ratio can be achieved for fiberglass struts than for any metallic struts, and that integrally-wrapped metallic end fittings can be used to achieve axial load transfer without reliance on bond strength or mechanical fasteners. |
| NASA分類 | MATERIALS, NONMETALLIC |
| レポートNO | 72N33564
NASA-CR-120937
LMSC-D281476 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/202172 |
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