FIELD: rocketry and space engineering; spacecraft with descent vehicle for transportation of crew to space and return to Earth. SUBSTANCE: proposed spacecraft includes engine compartment and coupling unit in addition to descent vehicle. Nose section of descent vehicle is mounted on engine compartment and coupling unit is mounted on bottom portion of descent vehicle. Coupling unit, compartment and descent vehicle are coaxial relative to one another. Crew seats located in case of descent vehicle are turnable through small angle relative to transversal plane of spacecraft in way of its nose section. EFFECT: improved arrangement and operating properties; extended functional capabilities. 8 dwg
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