FIELD: space technology.
SUBSTANCE: invention relates to reusable space aircraft (RSA) flying in space both around the Earth and in interplanetary space. The RSA contains three stages, each of which consists of eight modules, twelve lifting propeller power plants (LSPP) with in-flight folding propellers located in the upper part of the power modules, the rotation of the blades of which from vertical to horizontal position and vice versa is carried out by mechanisms, solid-fuel rocket engines (SFRE), including acceleration and braking, eight turbofan engines (TFE) with fuel tanks installed at the bottom of the power modules of stage I, aerodynamic surfaces installed on all stages to create lifting power with diving rudders and aerodynamic surfaces with jaw rudders, docking devices for connecting the stages to each other and access through the door hatch of the retractable telescopic tube from the lower stage I to the upper stage III when getting through an access tube installed in each central module, landing devices of stage I and landing devices of stages II and III, which are installed on each stage from the bottom of power modules equipped with LSPP.
EFFECT: expansion of the range of solutions to build reusable space aircraft.
1 cl, 7 dwg
