| タイトル | Launch Vehicle Design Process: Characterization, Technical Integration, and Lessons Learned |
| 本文（外部サイト） | http://hdl.handle.net/2060/20010066713 |
| 著者（英） | Schutzenhofer, L. A.; Humphries, W. R.; Blair, J. C.; Ryan, R. S. |
| 著者所属（英） | NASA Marshall Space Flight Center |
| 発行日 | 2001-05-01 |
| 言語 | eng |
| 内容記述 | Engineering design is a challenging activity for any product. Since launch vehicles are highly complex and interconnected and have extreme energy densities, their design represents a challenge of the highest order. The purpose of this document is to delineate and clarify the design process associated with the launch vehicle for space flight transportation. The goal is to define and characterize a baseline for the space transportation design process. This baseline can be used as a basis for improving effectiveness and efficiency of the design process. The baseline characterization is achieved via compartmentalization and technical integration of subsystems, design functions, and discipline functions. First, a global design process overview is provided in order to show responsibility, interactions, and connectivity of overall aspects of the design process. Then design essentials are delineated in order to emphasize necessary features of the design process that are sometimes overlooked. Finally the design process characterization is presented. This is accomplished by considering project technical framework, technical integration, process description (technical integration model, subsystem tree, design/discipline planes, decision gates, and tasks), and the design sequence. Also included in the document are a snapshot relating to process improvements, illustrations of the process, a survey of recommendations from experienced practitioners in aerospace, lessons learned, references, and a bibliography. |
| NASA分類 | Launch Vehicles and Launch Operations |
| レポートNO | M-1018
NAS 1.60:210992
NASA/TP-2001-210992 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/92815 |
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