AUTOMATIC CLOSING DEVICE IN ROCKET CHAMBER FOR LAUNCHER CELL FOR A PLURALITY OF MISSILES

    公开(公告)号:JPH04344099A

    公开(公告)日:1992-11-30

    申请号:JP781092

    申请日:1992-01-20

    Abstract: PURPOSE: To prevent an exhaust gas from flowing inversely into a cell space that is located at the upstream side of the nozzle outlet of a rocket and from being recirculated. CONSTITUTION: An exhaust gas management system for a missile discharge device with a plurality of launch cells 74 for evacuating into a common plenum 86 is provided with an aft closure member 78 that is helpful for closing the channel of an exhaust gas to a non-actuated cell while opening passage of the exhaust gas from an active cell during missile combustion is being formed.

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