FIELD: space equipment.
SUBSTANCE: invention relates to space engineering, particularly, to reusable spacecrafts. Manned or unmanned reusable carrier rocket includes module with cruise rocket engines, lateral accelerating modules and integrated control system. Lateral radial engines are used in vertical landing mode to create stable total balancing reactive moment relative to center of gravity of lower part of carrier rocket and to ensure flight in dense layers of atmosphere. Engines are made by turbojet two-circuit turbojet engines or turbojet two-circuit turbojets with afterburner. During operation of mid-flight rocket engines in upper layers of atmosphere, inlet openings of air intakes for engines of turbojet engine or turbojet engine are closed with retractable fairings.
EFFECT: reusable transport space system is achieved.
1 cl, 51 dwg
