Self-activated rocket launcher cell closure

Ordnance – Rocket launching – Having tubular guide means

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Details

89 1816, 89 1812, F41F 304

Patent

active

051626055

ABSTRACT:
A structural arrangement is provided in conjunction with the upper closure of a missile cell which, upon launch of the missile, generates a rarefaction wave which assists in closing the bottom closure of the missile cell. As a result, reverse flow of exhaust gases back up into the missile chamber from an associated plenum chamber is prevented or minimized.

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