| タイトル | Configuration evaluation and criteria plan. Volume 1: System trades study and design methodology plan (preliminary). Space Transportation Main Engine (STME) configuration study |
| 本文（外部サイト） | http://hdl.handle.net/2060/19870009171 |
| 著者（英） | Bair, E. K. |
| 著者所属（英） | Aerojet Technical Systems Co. |
| 発行日 | 1986-08-01 |
| 言語 | eng |
| 内容記述 | The System Trades Study and Design Methodology Plan is used to conduct trade studies to define the combination of Space Shuttle Main Engine features that will optimize candidate engine configurations. This is accomplished by using vehicle sensitivities and engine parametric data to establish engine chamber pressure and area ratio design points for candidate engine configurations. Engineering analyses are to be conducted to refine and optimize the candidate configurations at their design points. The optimized engine data and characteristics are then evaluated and compared against other candidates being considered. The Evaluation Criteria Plan is then used to compare and rank the optimized engine configurations on the basis of cost. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 87N18604
NASA-CR-178939
DR-9-VOL-1
NAS 1.26:178939
RPT/BB0324-VOL-1 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/151645 |
