FIELD: rocket equipment.
SUBSTANCE: invention relates to rocket engineering and can be used in development of multiple rocket launchers with large combat elements. Cartridge head part of jet projectile comprises fairing, shell, successive payload elements with boost assembly and piston connected by means of accumulating cavities. At that payload elements are supported by L-shaped adapter with length of 9 gauges and fairing. Cone cover of parachute container of payload is coaxially fixed in housing, forming opening mechanism located along axis of rotation. On the piston there is a gas outlet channel with a reflector oriented towards the accumulating cavity.
EFFECT: improving operating reliability of head part at separation of missile flight trajectory.
1 cl, 4 dwg
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Authors
Dates
2019-07-15—Published
2018-10-01—Filed