| タイトル | Study of solid rocket motors for a space shuttle booster. Volume 2, book 1: Analysis and design |
| 本文（外部サイト） | http://hdl.handle.net/2060/19720015125 |
| 著者所属（英） | Lockheed Propulsion Co. |
| 発行日 | 1972-03-15 |
| 言語 | eng |
| 内容記述 | An analysis of the factors which determined the selection of the solid rocket propellant engines for the space shuttle booster is presented. The 156 inch diameter, parallel burn engine was selected because of its transportability, cost effectiveness, and reliability. Other factors which caused favorable consideration are: (1) recovery and reuse are feasible and offer substantial cost savings, (2) abort can be easily accomplished. and (3) ecological effects are acceptable. |
| NASA分類 | PROPULSION SYSTEMS |
| レポートNO | 72N22775
NASA-CR-123620
LPC-629-6-VOL-2-BK-1 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/203592 |
