Destruction of rocket engines

Furnaces – Refuse incinerator – For explosive or radioactive material

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Details

110242, 588202, F23G 700

Patent

active

054580714

ABSTRACT:
An installation for the destruction of solid fuel rocket engines. The installation comprises a pressure and temperature resistant vessel having a neck portion and a gas chamber portion with heat dissipating means. In operation the rocket engine is gripped in the neck portion and upon ignition of the solid fuel combustion gases are discharged into the gas chamber. Means are provided for the controlled discharge of combustion gases into a gas disposal device.

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