| タイトル | Development of a new generation solid rocket motor ignition computer code |
| 本文（外部サイト） | http://hdl.handle.net/2060/19940024297 |
| 著者（英） | Jenkins, Rhonald M.; Foster, Winfred A., Jr.; Ciucci, Alessandro; Johnson, Shelby D. |
| 著者所属（英） | Auburn Univ. |
| 発行日 | 1994-02-10 |
| 言語 | eng |
| 内容記述 | This report presents the results of experimental and numerical investigations of the flow field in the head-end star grain slots of the Space Shuttle Solid Rocket Motor. This work provided the basis for the development of an improved solid rocket motor ignition transient code which is also described in this report. The correlation between the experimental and numerical results is excellent and provides a firm basis for the development of a fully three-dimensional solid rocket motor ignition transient computer code. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 94N28800
NASA-CR-195734
NAS 1.26:195734 |
| 権利 | No Copyright |
