FIELD: instantaneous separation of structural components in rocketry and space engineering; aviation; oil industry.
SUBSTANCE: proposed device has body secured on separable component, electric detonators mounted in body and elongated detonating charges. One elongated detonating charge is received by bore in body and other is received by body in shield located in body for motion along its longitudinal axis. Body is provided with stop. Distance between shield and stop is no less than diameter of cross section of elongated detonating charge. Besides that, shield may be provided with locking member.
EFFECT: possibility of keeping surrounding instruments, components and other members intact.
2 dwg
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