METHOD FOR SEPARATION OF ROCKET SHOCK-ABSORBERS IN FLIGHT TRAJECTORY AND DEVICE FOR ITS REALIZATION

摘要

FIELD: submarine rocketry. SUBSTANCE: simultaneously with removal of rigid coupling between the rocket and shock-absorbers solid-propellant gas generator gets actuated, whose gases pressurize two flattened tubular elements, thus transforming the shock-absorbing belt into a ring of a larger diameter. After that the shock-absorbing belt comes off the rocket under the action of the air velocity flow and the thrust of the rocket engine installation. EFFECT: reduced quantity of objects falling on the submarine, improved conditions of shockless motion of rockets at salvo fire. 3 cl, 4 dwg