Abstract:The present paper considers utilization of rocket motor propellant grains
that consist of two propellants. The idea is to achieve approximately
neutral burning using an outer surface inhibited cylindrical shape and
complex contact surface between propellants. An existing propellant grain
with complex geometry has been analytically modeled in terms of
determination of evolution of corresponding burning surface areas. The
analytical and experimental results? diagrams of this grain have been fou… Show more
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