Methods and apparatus for a tandem divert and attitude control system
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United States of America Patent
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Aug 12, 2014
Grant Date -
Feb 3, 2011
app pub date -
Jan 29, 2010
filing date -
Jul 30, 2009
priority date (Note) -
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Abstract
An aeronautical vehicle includes at least one set of tandem divert thrusters incorporated into the body. Each set of tandem divert thrusters includes a first divert thruster and a second divert thruster, each configured to provide substantially equal thrust forces at substantially the same time and in substantially opposite directions such that the moment reference point lies between the first and second divert thrusters.
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