| タイトル | Liquid Rocket Booster (LRB) for the Space Transportation System (STS) systems study. Volume 2: Addendum 1 |
| 本文（外部サイト） | http://hdl.handle.net/2060/19910013053 |
| 著者所属（英） | Martin Marietta Aerospace |
| 発行日 | 1990-02-01 |
| 言語 | eng |
| 内容記述 | The potential of a common Liquid Rocket Booster (LRB) design was evaluated for use with both the Space Transportation System (STS) and the Advanced Launch System (ALS). A goal is to have a common Liquid Oxygen/Liquid Hydrogen (LO2/LH2) engine developed for both the ALS booster and the core stage. The LO2/LH2 option for the STS was evaluated to identify potential LRB program cost reductions. The objective was to identify the structural impacts to the external tank (ET), and to determine if any significant ET re-development costs are required as a result of the larger LO2/LH2 LRB. The potential ET impacts evaluated are presented. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 91N22366
NAS 1.26:184128
NASA-CR-184128 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/132890 |
