| タイトル | Liquid rocket booster study. Volume 2, book 6, appendix 10: Vehicle systems effects |
| 本文（外部サイト） | http://hdl.handle.net/2060/19900000822 |
| 著者所属（英） | General Dynamics Corp.|Eagle Engineering, Inc. |
| 発行日 | 1989-03-24 |
| 言語 | eng |
| 内容記述 | Three tasks were undertaken by Eagle Engineering as a part of the Liquid Rocket Booster (LRB) study. Task 1 required Eagle to supply current data relative to the Space Shuttle vehicle and systems affected by an LRB substitution. Tables listing data provided are presented. Task 2 was to evaluate and compare shuttle impacts of candidate LRB configuration in concert with overall trades of analysis activity. Three selected configurations with emphasis on flight loads, separation dynamics, and cost comparison are presented. Task 3 required the development of design guidelines and requirements to minimize impacts to the Space Shuttle system from all LRB substitution. Results are presented for progress to date. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 90N10138
NASA-CR-183605
NAS 1.26:183605 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/140377 |
