Patent attributes
Embodiments disclosed include a system comprising a missile segment having an external surface conforming to a portion of an external surface of a missile body. The missile segment comprising a plurality of chemical plasma dispensing units (CPDUs) having a chemical plasma reactant (CPR). Each CPDU is addressable so that a group of selected CPDUs in an area is ignited simultaneously to cause a first reaction to push CPR particles into a flow stream surrounding the missile body. The CPR particles to complete a second reaction in the flow stream over a reaction time period to effectuate production of expanding hot gas energy caused by heating air in the flow stream and gaseous reaction products over the missile body to provide an amount of a steering force to change one or more of six degrees of freedom at a location on the body. A missile and method are also provided.