| タイトル | Space Shuttle solid rocket booster initial water impact loads and dynamics - Analysis, tests, and flight experience |
| 著者（英） | Rawls, E. A.; Kiefling, L. A.; Kross, D. A.; Murphy, N. C. |
| 著者所属（英） | NASA Marshall Space Flight Center|Chrysler Corp. |
| 発行日 | 1983-01-01 |
| 言語 | eng |
| 内容記述 | A series of scale model tests, finite element dynamic response analyses and full scale segment tests have been performed for purposes of developing design criteria for the initial water impact loading conditions applied to the internal stiffener rings located in the aft skirt portion of the Space Shuttle Solid Rocket Booster (SRB). In addition, flight experience has yielded information relative to structural reinforcement requirements. This paper discusses the test and analysis methods and summarizes significant results. It is noted that, although scale model test data are valuable for identifying trends, they have shortcomings concerning definition of full scale design loads criteria. Also, the frequently used static equivalent loads definition approach is not applicable for this type impact loading condition applied to an aft skirt type structure. Various types of ring structural fixes, including the addition of selected types of foam, are presented as well as associated full scale segment test results. Depending on the type and contour shape of the foam, reductions on applied pressures and peak measured strains over 50 percent are noted. |
| NASA分類 | LAUNCH VEHICLES AND SPACE VEHICLES |
| レポートNO | 83A29858
AIAA PAPER 83-0956 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/404532 |
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