FIELD: space engineering; transportation of payloads for erection of bulky orbital complexes. SUBSTANCE: proposed method includes placing the payload used as members of load-bearing frame-work of launch vehicle case and made in form of long articles (truss, for example) between outer and inner skins of launch vehicle. After injection into orbit, launch vehicle case is dismantled using the payload for erection of bulky space structures. Stages of launch vehicle are connected in parallel pattern; their modules are arranged around case with payload. EFFECT: enhanced efficiency of delivery of long articles and structural members to orbit; reduced consumption of air in erection of bulky complexes in orbit. 2 dwg
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