RU2011132615A

RU2011132615A - SPACE HEAD

Info

Publication number: RU2011132615A
Application number: RU2011132615/11A
Authority: RU
Inventors: Виктор Николаевич Веселов; Светлана Львовна Козлова; Михаил Викторович Рожков
Original assignee: Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева"
Priority date: 2011-08-04
Filing date: 2011-08-04
Publication date: 2013-02-10
Also published as: RU2478533C1

Abstract

Космическая головная часть, состоящая из головного обтекателя и космического аппарата, отличающаяся тем, что в состав космической головной части введен промежуточный отсек, обеспечивающий с помощью разделяемых в полете соединений связь космического аппарата с ракетой-носителем и головным обтекателем, причем агрегатная часть космического аппарата размещена во внутренней полости промежуточного отсека и находится вне пределов зоны схода промежуточного отсека, отделяемого от космического аппарата вместе с ракетой-носителем, а в верхнем шпангоуте промежуточного отсека совмещены два торцевых разъемных соединения, разделяемых в полете, соединяющих этот отсек с головным обтекателем и с космическим аппаратом соответственно.The space head part, consisting of the head fairing and the spacecraft, characterized in that an intermediate compartment is introduced into the space head part, which ensures the communication of the spacecraft with the launch vehicle and the head fairing by means of the connections separated in flight, the aggregate part of the spacecraft being placed in the internal cavity of the intermediate compartment and is located outside the vanishing zone of the intermediate compartment, separated from the spacecraft along with the launch vehicle, and in the upper intermediate bulkhead compartment separable two end compound are combined, separated in flight connecting the compartment with the payload fairing with the spacecraft respectively.

Claims

The space head part, consisting of the head fairing and the spacecraft, characterized in that an intermediate compartment is introduced into the space head part, which ensures the communication of the spacecraft with the launch vehicle and the head fairing by means of the connections separated in flight, the aggregate part of the spacecraft being placed in the internal cavity of the intermediate compartment and is located outside the vanishing zone of the intermediate compartment, separated from the spacecraft along with the launch vehicle, and in the upper intermediate bulkhead compartment separable two end compound are combined, separated in flight connecting the compartment with the payload fairing with the spacecraft respectively.