Analysis of Interference Factors on Paralleling Multi-satellite Separation

At present, the majority of launches for multiple main satellites utilize a serial layout, which is associated with several issues such as high costs, reduced carrying capacity, and decreased separation reliability. To address these challenges, a parallel layout scheme is proposed for launching multiple main satellites. This scheme involves three main satellites separating simultaneously, with the separation device designed to maintain a certain speed difference between the satellites to ensure safe separation and short-term orbital safety. The proposed layout scheme is implemented in a specific type of multi-satellite launch mission and is subjected to extreme simulation analysis to calculate the worst-case scenarios that may arise during the separation process. The simulation results demonstrate that this separation scheme is capable of ensuring the safe separation of the satellite and rocket.