FIELD: solid-propellant rocket engines. SUBSTANCE: method includes heating by means of electric current supplied to electrode system and passed through reaction zone of combustion of condensed system. Electric field is formed in heated layer of condensed system which creates electric current. Constant electric contact is maintained between conduction zone and adjustable current source. Electrochemical regulation of kinetics of initial phases of combustion is effected through change of current magnitude by means of external control system. EFFECT: possibility of changing rate of combustion of condensed phase. 2 dwg
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