FIELD: aviation.
SUBSTANCE: invention relates to the spacecraft security measures (SM) from the high speed impact actions of space environment particles. The screen contains the honeycomb structure made of the corrugated metal mesh. The mesh corrugations are arranged parallel with a pitch in 2-3 times more than the mesh wire thickness. The height of the corrugations in 3-5 times increases the minimum characteristic size of the particles colliding with the spacecraft. The screen might be double layered with the second layer corrugations oriented perpendicular to the corrugations of the first layer.
EFFECT: increase of the spacecraft protection efficiency from the high speed particles by increasing the fragmentation degree of the particles without increasing the screen weight.
2 cl, 10 dwg
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Authors
Dates
2017-06-29—Published
2016-03-02—Filed