FIELD: space system engineering. SUBSTANCE: engine-rocket has craft with nozzle, small-size propellant tanks with rotary intakes propellant from light beam directed into rocket nozzle of stationary laser with feeders delivering explosive propellant materials in grains in form of elementary parts into beam. Nozzle is additionally furnished with pickups of laser beam position relative to nozzle coupled with rotary intakes. EFFECT: reduced energy losses at provision of supply of engine-rocket with explosive granulated material using variable beam of laser. 11 cl, 7 dwg
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