SOLID-PROPELLANT ROCKET ENGINE WITH VARIABLE ELECTROMAGNETIC CONTROL OF FUEL BURNING INTENSITY

摘要

FIELD: rocketry. ^ SUBSTANCE: invention relates to rocket engine installations with controlled process of fuel burning. Proposed solid-propellant rocket engine with variable electromagnetic control of fuel burning intensity has body, solid-propellant charge, control system, superhigh frequency generator and wave guide. Wave guide is made rectangular in form of one part integral with rocket engine body and is provided with slit radiators closed by fusible metal foil. ^ EFFECT: provision of control of intensity of burning of solid-propellant charge to increase or decrease burning intensity. ^ 1 dwg