FIELD: transport.
SUBSTANCE: invention relates to rocket-and-space engineering and can be used for spacecraft rescue in hazard situations. Emergency rescue system includes upper stage engines, pyrotechnic catapulting missile working stages separation subsystem based on device containing several shafts connected by synchronising ring-shaped gas channel with rods, pyro cartridges with electric detonators and substance providing smooth gradual detonation, shock absorbers for dynamic impact amortisation.
EFFECT: lower mass of missile.
6 dwg
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