FIELD: space engineering; positioning several satellites 12 on launch vehicle 10 and simultaneous injection of these satellites. SUBSTANCE: device includes strut 18 adaptable for launch vehicle and identical coupling members 20. Each member is provided with satellite attachment and separation system and electrical connectors for electrical connection with launch vehicle and coupling members. Identical mounting seats are provided on the outside of strut 18. Coupling members 20 may be mounted on each of these seats. EFFECT: possibility of unification of satellite injection equipment; enhanced guarantee of launching satellites in scheduled time. 9 cl, 9 dwg
