摘要
In order to improve the launch coefficient as the goal, a systems engineering technology is proposed. Combined with the design object, the overall multi-level design process and optimization object are sorted out from the four aspects of design concept, constraint boundary, design method, and identification return, to build the overall system of technologies. Taking the system as the traction, combined with the development practice of the new generation of launch vehicles, the research process and application effects of some of the technologies such as safety margin shooting, active environmental control, multi-disciplinary joint optimization, and propellant residue identification are summarized. At the same time, the direction of follow-up and continuous research is pointed out, which is of great significance to support the improvement of the launch coefficient.
| 投稿的翻译标题 | Systems Engineering Technology for Launch Coefficient Improvement |
|---|---|
| 源语言 | 繁体中文 |
| 页(从-至) | 322-333 |
| 页数 | 12 |
| 期刊 | Yuhang Xuebao/Journal of Astronautics |
| 卷 | 44 |
| 期 | 3 |
| DOI | |
| 出版状态 | 已出版 - 3月 2023 |
| 已对外发布 | 是 |
关键词
- Identification and regression
- Launch coefficient
- Launch vehicle
- Optimal control
- Probability design
指纹
探究 '面向运载系数提升的总体技术' 的科研主题。它们共同构成独一无二的指纹。引用此
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