Combined steering and drag-reduction device
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United States of America Patent
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Nov 22, 2016
Grant Date -
Oct 1, 2015
app pub date -
Oct 21, 2013
filing date -
Oct 22, 2012
priority date (Note) -
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status (Latency Note)
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Abstract
A combined steering and drag reduction device for a missile is disclosed. The device includes a base and an upper part which are arranged in succession along a main axis of navigation of the missile. Advantageously, the device also includes a pressurized-gas generator and at least one lateral thruster having at least one nozzle configured to deliver a thrust, by expanding gas transmitted by the generator and oriented along an axis substantially perpendicular to the main axis. The at least one lateral thruster also has at least one stabilizing chamber configured to expand the gas transmitted by the generator and expel it through an outlet section of the base substantially perpendicular to the main axis.
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