FIELD: aircraft engineering.
SUBSTANCE: deployable decelerator consists of rigid front shield with flexible shell secured thereto and coated with resilient heat-isolated jacket from outer side. Tight resilient torus-shape shells are arranged inside flexible shell. Gas cylinders of torus-shape shell inflation are arranged at inner surface of rigid front shield. Walls of torus-shape shell walls have outer sealed layer and inner elastic layer to be hardened after deployment and pressurisation of shells by gas mix components.
EFFECT: higher dynamic stability and reliability.
3 cl, 2 dwg
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