Recoilless launching
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United States of America Patent
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Nov 30, 2010
Grant Date -
N/A
app pub date -
Sep 22, 2009
filing date -
Jun 10, 2005
priority date (Note) -
Expired
status (Latency Note)
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Abstract
An arrangement for recoilless launch including a non-gaseous reaction mass having a weight in a range of about 25% to about 75% of a weight of a projectile. For the same projectile energy, less propellant is required than a rocket, which minimizes backblast and reduces before-launch weight. The recoilless launching is adapted to shoulder-launched projectiles in a confined space. The reaction mass may be particles associated with a propellant so as to be released concurrently as the propellant turns into gas and accelerated by and with the propellant gas in a nozzle.
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