FIELD: rocketry and space engineering; injection of orbital space vehicles into near-earth orbit. SUBSTANCE: nose unit is provided with adapter rigidly secured on side of open end of nose fairing envelope; payload attachment units are located on adapter and attachment unit for securing with rocket is fastened with nose fairing. Prior to connecting the nose unit to launch vehicle, payload is coupled to adapter after which it is closed with nose fairing and adapter is coupled to nose fairing on side of open end. Nose unit thus assembled is coupled to launch vehicle over end of nose fairing. EFFECT: protection against external action at autonomous ground operation, at coupling with launch vehicle and on active trajectory leg. 6 dwg
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