Method and apparatus for launch recoil abatement
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United States of America Patent
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Feb 24, 2015
Grant Date -
Mar 20, 2014
app pub date -
Jan 11, 2013
filing date -
Jan 12, 2012
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Abstract
Recoil forces of a launched missile and the moment force imposed on the launch platform can be reduced by use of a recoil abatement element in communication with a launch tube. The recoil abatement element includes at least one nozzle configured to receive therethrough exhaust gasses from a missile when launched. The nozzle can be canted or otherwise configured to direct the exhaust gasses in a desired direction to thereby offset moment force imposed on the platform by the exhaust gasses.
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