FIELD: engines.
SUBSTANCE: invention relates to rocket propulsion systems and is intended for use as a multi-matrix multi-vector reconfigurable propulsion system of small-size spacecrafts. System contains three compactly embedded one into another cylinder-shaped monolithic heat-resistant dielectric (MHD) substrates with a matrix organization of an ordered array of motor cells consisting of solid-propellant motor elements ranged in different directions. System comprises a bar for linear movement, a reversible step motor and spherical igniters. Control is carried out through switches, decoders, memory units and a controller.
EFFECT: possibility of reconfiguration of nested cylindrical MHD substrates with matrix structures of motor cells with multi-vector directions of rods arranged in an orderly manner on their surfaces.
1 cl, 5 dwg
