| 摘要 |
The invention relates to rocket engineering, in particular to system of stabilization of rockets where stabilizers are used that are opened or unfolded after launch. In stabilization system each stabilizer is arranged in plan view in the form of polygon inscribed to semi-circle with center on the lower frame of the body of tail compartment tangent to surfaces of the lower bottom of rocket engine and jet in meridian plane and restricted with surfaces of the body and tail compartment and the jet, at that the drive of unfolding of each stabilizer and springy mechanism that holds it in infolded state are arranged as continuous two-side torsion spring symmetrical with respect to place of symmetry of stabilizer, fixed with the ends on articulated joint and closed through elongated turn as carrier with possibility of its interaction with core chord of stabilizer and rotation with respect to axis of hinged unit that goes through the center of the semi-circle. Set of stabilizers has more than sixteen stabilizers. |
