FIELD: process engineering.
SUBSTANCE: invention relates to rocketry, particularly, to plant intended for removal of composite solid propellant from compact rocket engine case, said solid propellant being based on synthetic rubber, ammonium perchlorate and aluminium powder. Proposed plant intended for removal of composite solid propellant from compact rocket engine case comprises heating station, pump, shutoff valves and accessories, control instruments, sealed apparatus furnished with covers and insulated heating jacket, water solution preparation reactor, car with support, tray, cylinder with piston, oil station with hydraulic cylinder communicated via control slide valve with oil feed pump, and used solution tank.
EFFECT: safe removal, reused of rocket engine case.
2 dwg
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