Lin Song Zhang Yuzhu (Beijing University of Aeronautics and Astronautics School of the Astronautics,Beijing100083)
Based on the experiments and theoretical analysis, a simplified spacecraft shield design method is developed in this paper, to choose the shield style and begin the preliminary spacecraft shield design A supposed metal particle is produced as the "design" particle to equate the effect made by realized debris The semi-empirical geometrical formulation for specific shield and the orbital debris engineering environment model are also utilized to roughly size the bumper and rear wall of meteoroid/debris shields The results of Whipple Shielding are consistent with that of other methods, so this design method developed is efficient and applied for the realized engineering design work.
Lin Song Zhang Yuzhu (Beijing University of Aeronautics and Astronautics School of the Astronautics,Beijing100083). Simplified Design Method for the Spacecraft Shield Structure[J]. .
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