The invention relates to the technical field of
rocket single-
machine vibration reduction, and discloses a
rocket single-
machine vibration reduction device, a carrier
rocket and a rocket single-
machine vibration reduction method.The rocket single-
machine vibration reduction device comprises a connecting piece, a first vibration reduction
assembly and a second vibration reduction
assembly, a first connecting hole is formed in a single machine, and the connecting piece penetrates through the first connecting hole and is detachably connected with a support; the first vibration reduction
assembly comprises a first
axial vibration reduction pad and / or a first lateral vibration reduction pad, the second vibration reduction assembly comprises a second lateral vibration reduction pad and a first limiting pad which are arranged on the periphery of the connecting rod in a sleeving mode, and a first
flange is arranged on the periphery of the first limiting pad in the single machine direction in an extending mode. The carrier rocket comprises the rocket stand-alone damping device. The rocket single
machine vibration reduction method comprises the steps that a target single machine and a target support are assembled, the installation frequency of the target single machine is obtained and compared with the preset installation frequency, and a first
axial vibration reduction pad and a first lateral vibration reduction pad are increased or decreased according to the comparison value. And the damping effect is good, and follow-up adjustment and optimization are facilitated.