FIELD: rocketry. SUBSTANCE: rocket includes boosters of launch vehicle stages with intermediate spacer between them. Lower part of booster of final stage includes propellant tank with engine plant. This part is secured in intermediate spacer on booster of next-to-final stage by means of flexible spacer which consists of two sections of envelope: cylindrical and conical at taper angle of 50 to 70 deg. Upper part of booster of final stage projects from intermediate spacer. EFFECT: reduced level of dynamic loading of payload. 2 cl, 1 dwg
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