Process and plant for destroying solid-propellant rocket motors

Ammunition and explosive-charge making – Bomb disposal

Reexamination Certificate

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Details

C588S403000

Reexamination Certificate

active

10855322

ABSTRACT:
Described is a process and a plant for destroying rocket motors, including in particular the following steps and stations: cutting of the motor into sections; cooling of the sections containing propellant by immersion in a cryogenic liquid; and fragmenting and extraction of the cooled propellant by elastic deformation of the casing of the section. The propellant fragments are recovered for subsequent treatment and the casings are deactivated before being scrapped.

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patent: 2002048499 (2002-02-01), None
patent: 2143660 (1999-12-01), None
English translation of RU 2143660 C1, Dec. 1999, Russia, Borozdin et al.
English translation of JP 2002048499 A, Feb. 2002, Japan, Funahashi et al.

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