FIELD: space equipment.
SUBSTANCE: invention relates to space engineering, namely to means of damping loads on spacecraft during landing. System of damping loads on spacecraft when landing on atmospheric-free objects comprises soft U-shaped in cross section shell made of mail mesh. Net forms a toroid filled with filler in the form of granular, solid-state and spherical elements. Diameter of elements is 0.012–0.015 m, they are laid in 12–15 layers in said shell. Weight of the filler shall be 15 ± 5 % of the weight of the spacecraft.
EFFECT: higher reliability of spacecraft when landing.
1 cl, 4 dwg
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