DEPLOYABLE DECELERATOR FOR DESCENT IN ATMOSPHERE OF PLANETS

摘要

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