摘要
研究了挤压式液体推进剂空间发动机系统布局对空间飞行器质心漂移的影响，提出了质心漂移的计算模型，得到了对发动机系统布局有指导作用的结论。
ffect of arrangements of a pressure-feed, liquid propellant space engines system on centroid drift of a spacecraft was studied in this paper. A mathmematical model for calculation of the centroid drift was given.Some important conclusions of the arrangements for a liquid propellant space engines system were obtained.
出处
《中国空间科学技术》
CSCD
北大核心
1996年第6期50-53,共4页
Chinese Space Science and Technology
