DEVICE FOR SEPARATION OF BALLISTIC MISSILE SECTION Russian patent published in 1999 - IPC

FIELD: rocket manufacturing. SUBSTANCE: the device uses a self-contained powder rocket engine and a mechanism for elimination of rigid coupling between the section and missile located in the section body. The engine nozzle is oriented relative to the section outside in radial direction at an angle to the section longitudinal axis determined from relationship: α = arctgL•r/J/m+L²,, where: r-section radius, m-section mass, J-section rolling moment, L-distance between the point of intersection of the nozzle longitudinal axis with the section outer surface and the projection of the center of masses onto the external generator of its surface. EFFECT: reduced mass and overall dimensions. 1 dwg