Self-actuating rocket chamber closures for multi-missile launch cells
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United States of America Patent
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Aug 11, 1992
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N/A
app pub date -
May 13, 1991
filing date -
May 13, 1991
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Abstract
An exhaust gas management system for missile launch arrangements having multiple launch cells exhausting into a common plenum includes automatic aft closure members which serve to close off the flow passages to inactive cells while providing an open passage for exhaust gases from an active cell undergoing a missile firing. This arrangement prevents back flow or recirculation of exhaust gases into the volume in the cell which is upstream of the rocket nozzle exit.
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