中国航天（英文版）2016，Vol.17Issue(4)：14-20,7.
Parameters and Trajectory Overall Optimization Design of the Combined Cycle Engine Reusable Launch Vehicle
Parameters and Trajectory Overall Optimization Design of the Combined Cycle Engine Reusable Launch Vehicle
CUI Naigang 1ZHAO Lina 2HUANG Rong 1WEI Changzhu2
作者信息
- 1. School of Astronautics of Harbin Institute of Technology, Harbin 150001
- 2. China Academy of Launch Vehicle Technology, Beijing 100076
- 折叠
摘要
关键词
Reusable launch vehicle/Combined cycle engine/Bilevel hierarchical/Integrated/Parameters/trajectory overall optimizationKey words
Reusable launch vehicle/Combined cycle engine/Bilevel hierarchical/Integrated/Parameters/trajectory overall optimization引用本文复制引用
CUI Naigang,ZHAO Lina,HUANG Rong,WEI Changzhu..Parameters and Trajectory Overall Optimization Design of the Combined Cycle Engine Reusable Launch Vehicle[J].中国航天（英文版）,2016,17(4):14-20,7.
