ROCKET ENGINE OF IMPULSE VERNIER UNIT

摘要

FIELD: rocketry.;SUBSTANCE: invention relates to impulse-type rocket engines with small time of operation and considerable loads acting onto charge. Proposed rocket engine of impulse vernier unit has body, solid-propellant change in form of charge tube cluster, igniter arranged in head part of engine, and nozzle. Tubes are held on carrying plate in head part of engine by cap of cylindrical pins connected pins connected with channel of charge tubes. Odd number of parallel slots is made on carrying plate for arrangement of pins in opposite directions.;EFFECT: improved reliability and mass perfection of vernier unit.;4 cl, 3 dwg