|
|||||
|
|
A multi-objective,multidisciplinary design optimization methodology for the conceptual design of a spacecraft bi-propellant propulsion system |
|
| Authors: | H R Fazeley H Taei H Naseh M Mirshams |
| Abstract: | |
| Keywords: | |
| 本文献已被 SpringerLink 等数据库收录！ | |
|
||||||||||||||||
|
||||||||||||||||
|
||||||||||||||||
|
|
|
|
| 设为首页 | 免责声明 | 关于勤云 | 加入收藏 |
|
Copyright©北京勤云科技发展有限公司 京ICP备09084417号-23 |
