The electric propulsion feasibility and effect in space debris mitigation were studied.

研究了电推进在静止轨道空间碎片减缓中应用的可行性和效果.

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Because the spacesuit protection only 1 mm in diameter, about the impact of space debris.

因为航天服只能防护直径在1毫米左右的空间碎片撞击.

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The cumulative damage area on K 8 glass was obtained by space debris distribution models of ORDEM 2000.

利用ORDEM2000碎片分布模型估算了K8玻璃累积损伤面积.

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