FIELD: aeronautical and space engineering.
SUBSTANCE: proposed system has set of inflatable envelopes, devices for securing the system to module, container, surfaces protecting the inflatable envelopes, elastic and/or rigid lines for securing to module, system for placing the inflatable envelopes in operating position and system for control of pressure inside envelopes. Module protective surfaces have rhomboid or cone-shaped form; they open at hypersonic speeds.
EFFECT: enhanced accuracy of landing.
6 cl, 10 dwg
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