| タイトル | Technical report analysis and design: Study of solid rocket motors for a space shuttle booster, volume 2, book 1, supplement 1 |
| 本文（外部サイト） | http://hdl.handle.net/2060/19730008042 |
| 著者所属（英） | Lockheed Propulsion Co. |
| 発行日 | 1972-05-02 |
| 言語 | eng |
| 内容記述 | An analysis and design effort was conducted as part of the study of solid rocket motor for a space shuttle booster. The 156-inch-diameter, parallel burn solid rocket motor was selected as its baseline because it is transportable and is the most cost-effective, reliable system that has been developed and demonstrated. The basic approach was to concentrate on the selected baseline design, and to draw from the baseline sufficient data to describe the alternate approaches also studied. The following conclusions were reached with respect to technical feasibility of the use of solid rocket booster motors for the space shuttle vehicle: (1) The 156-inch, parallel-burn baseline SRM design meets NASA's study requirements while incorporating conservative safety factors. (2) The solid rocket motor booster represents a cost-effective approach. (3) Baseline costs are conservative and are based on a demonstrated design. (4) Recovery and reuse are feasible and offer substantial cost savings. (5) Abort can be accomplished successfully. (6) Ecological effects are acceptable. |
| NASA分類 | PROPULSION SYSTEMS |
| レポートNO | 73N16769
NASA-CR-124002
LPC-629-6-VOL-2-BK-1-SUPPL-1 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/200765 |
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