ROCKET LAUNCH UNIT Russian patent published in 2021 - IPC F42B10/66 F02K1/00 F02K9/80 

FIELD: space technologies.

SUBSTANCE: invention relates to rocket technology, in particular to rocket launching devices. The launch unit of the rocket contains an annular body, a launch engine with a jet nozzle, a device for deflecting the thrust vector, a mounting unit to the rocket, and a correction system. The correction system includes a gas generator, a gas distribution device, a gas-dynamic actuating element and a control system. The launch of the rocket is provided using a transport and launch container. The launch unit is equipped with a tubular asymmetric nozzle covering the jet nozzle and made with the possibility of rotation around the longitudinal axis and subsequent fixation to ensure a given direction of flight of the rocket. The control system is able to receive a flight task. With the help of a gas distribution device, it is possible to correct the position of the rocket on the trajectory. The launch block is designed with the possibility of separation from the rocket due to the activation of the attachment unit of this block from the pressure of the combustion products of the main engine of the rocket after its launch. An annular obturator is mounted on the outer surface of the annular housing.

EFFECT: invention makes it possible to simplify the design, increase the reliability of operation, safety and technical and economic characteristics.

2 cl, 1 dwg