UNIVERSAL SPACE ROCKET SYSTEM FOR HIGH-CAPACITY TRANSPORT SYSTEMS Russian patent published in 2024 - IPC B64G1/00 

FIELD: rocket and space technology.

SUBSTANCE: invention is used for launching large-sized heavy (up to 50 tons) spacecrafts and stations into geostationary orbit, lunar orbit or for flights to Mars and other objects in deep space. The proposed rocket complex consists of a space rocket with sectional fuel tanks, a transport and installation vehicle, a launch facility and an assembly facility. The assembly facility is equipped with a technological workstation for wrapping the outer surface of the space rocket tanks with reinforcing thermoplastics and additional thermal insulation. The launch facility is designed for maximum mechanical and gas-dynamic thermal loads, based on the possible use of liquid propulsion systems (LPS) with oxygen + hydrogen or oxygen + methane components at the same levels of placement of the space rocket service sites. The transport and installation vehicle is equipped with the space rocket loading control system that monitors the size of the gaps between the contact surfaces and other parameters of the space rocket installation.

EFFECT: increasing the efficiency of missile systems that are universal in terms of servicing space rockets with existing and future rocket launchers.

1 cl, 4 dwg