摘要
一般用爆轰法使卫星与整流罩分离,一般不允许爆轰产物泄露而污染卫星表面.本文运用爆轰气体动力学,气溶胶基本理论,通过计算机模拟,分别预测陆地和太空星箭分离时,万一有爆轰产物泄露对卫星表面的污染量.
The explosion process is usually used for satellite releasing during fairing separation. Explosion products are not allowed to be leaked from the detonating tube connecting two parts of the fairing during the fairing separation process. This paper predicts the contamination of the explosion products falling on the satellite surface during fairing separation on the ground and in space in case of the computer simulation by using the theory of explosion gaseous dynamics and the basic theory of aerosol mechanics.
出处
《应用数学和力学》
EI
CSCD
北大核心
1993年第5期425-433,共9页
Applied Mathematics and Mechanics
关键词
卫星
表面
爆轰
气溶胶
污染量
satellite surface, explosion, jet flow, aerosol, the amount of dust