FIELD: rocket technics.
SUBSTANCE: group of inventions relates to aerospace engineering. Transfer compartment of the head part of a carrier rocket (CR) includes a housing, an adapter and a device for connection of the housing with the adapter. Device for connection of the housing with the adapter is made as arranged inside the housing frames, each of which comprises two arms, two rods and a support assembly. On the support assembly of each of the frames first ends of the arms and the rods of the frame are fixed. Second ends of the rods are fixed on the upper end frame of the housing, and second ends of the arms - on the lower end frame of the housing. Adapter is made of sections rigidly interconnected with brackets, each of which comprises the top and the bottom support sites, herewith the top support site is made with the possibility of connection with the payload, and the bottom support site with a detachable connection is connected to the support assembly of one of the frames. Transfer compartment housing is made in the form of a truncated cone or a cylinder.
EFFECT: technical result of the group of inventions is reduction of weight of the CR transient compartment.
18 cl, 28 dwg
Title | Year | Author | Number |
---|---|---|---|
CARRIER ROCKET TRANSFER COMPARTMENT AND ITS SUPPORTING FRAME | 2017 |
|
RU2661631C1 |
CARRIER ROCKET TRANSIENT COMPARTMENT AND TRUSS | 2018 |
|
RU2697493C1 |
ROCKET BOOSTER | 2009 |
|
RU2412871C1 |
DEVICE FOR GROUP LAUNCH OF SATELLITES AND REINFORCED FRAME | 2020 |
|
RU2725824C1 |
FORMER | 2018 |
|
RU2694486C1 |
TRANSITIONAL TRUSS | 2021 |
|
RU2779010C1 |
ADAPTER FOR WAY LOOSE OF USEFUL LOAD | 2016 |
|
RU2624959C1 |
DEVICE FOR GROUP LAUNCHING OF SATELLITES | 2019 |
|
RU2724000C1 |
SPACESHIP HEAD | 2011 |
|
RU2478533C1 |
SERVICE SYSTEM MODULE | 2015 |
|
RU2621221C1 |
Authors
Dates
2016-12-10—Published
2015-08-06—Filed