FIELD: transport.
SUBSTANCE: invention relates to space engineering. Proposed system comprises rocket stages with propellant tanks and oxidiser (oxygen) tanks, sustainer rocket engines and stabilisation and orientation engines. First stage features cylindrical shape and is equipped with aft section, adapter and cowl. Sustainer rocket engines run on hydrogen. Tanks of both stages represent bearing structures with combined bottoms. Second stage is shaped to truncated cone with spherical bottoms is equipped with thermal protection. Both stages are equipped with landing supports.
EFFECT: increased payload.
4 dwg
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