| タイトル | Structural design of integral tankage for advanced space transportation systems |
| 著者（英） | Davis, R. B.; Macconochie, I. O.; Lemessurier, R. W. |
| 著者所属（英） | NASA Langley Research Center|Kentron International, Inc. |
| 発行日 | 1982-01-01 |
| 言語 | eng |
| 内容記述 | Fully reusable launch vehicle concepts being studied for post-Shuttle era transports present major challenges for the structural design of large propellant tankage. The dominant structural elements are internal tankage for both cryogenic and non-cryogenic propellants which must operate in a broad range of thermal environments while meeting requirements for low weight and reusability. Several approaches to integral tank design are discussed and an analysis of a hot structure honeycomb sandwich tank for a circular body vehicle is presented. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 82A30132
AIAA PAPER 82-0634 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/411023 |
