Abstract
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.
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Communicated by Chien Wei-zang
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Zhen-kan, H., Shi-hong, W., Li-xing, Y. et al. The study of surface dust concentration of satellite in fairing separation. Appl Math Mech 14, 449–458 (1993). https://doi.org/10.1007/BF02453766
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DOI: https://doi.org/10.1007/BF02453766