FIELD: astronautics.
SUBSTANCE: group of inventions relates to spacecraft. Manned or unmanned reusable launch vehicle includes a central module with jet cruise engines located in tail part of central module, central or radially located side accelerating modules of one or several stages, integrated control system with communication with global positioning system, heat-resistant heat protection system. In the tail part of the second stage of the central module of the launch vehicle in the start and acceleration mode one or more manned or unmanned separated acceleration modules are fixed with jet cruise engines located in the tail part of the separating accelerating modules and at least with three lateral jet engines installed on end sections of radial wings-pylons of separated accelerating modules. At least at three end sections of radial wings-pylons or at least on three extending radial consoles side jet engines are installed.
EFFECT: higher stability and reliability of launch vehicle.
5 cl, 34 dwg
