FIELD: transport.
SUBSTANCE: invention relates to rocketry. Proposed rocket comprises first stage central module with first stage lateral modules and second stage central module with second stage lateral modules. Lateral modules are connected with central module by correction bars that may be disconnected. All modules have body, oxidiser and fuel tanks arranged there inside, liquid-propellant rocket engine in every module and systems to feed fuel components from lateral modules into central module. Rocket incorporates sets of roll nozzles including two opposed roll nozzles. Said sets are located on outer surface of lateral module bodies of all stages, remote from carrier rocket axis.
EFFECT: higher safety and controllability.
6 cl, 14 dwg
