FIELD: space technology.
SUBSTANCE: group of inventions relates to the field of space technology, and more specifically to block-modular spacecraft. The block-modular spacecraft body includes a service systems module (SSM) with a central part in the form of a cylindrical power structure (PS) and a payload module (PM) consisting of panels. The PM is mounted on a cylindrical PS, coaxial with a cylindrical SSM PS, which are separated by a horizontal panel of the PM. The latter is connected to a U-shaped spatial structure and is designed to connect cylindrical PM and SSM PSs into a single cylindrical spacecraft PS. Along the cylindrical PM PS, parallel to the XOZ plane, two rigidity support panels can be located, which are connected to the cylindrical PM PS by a horizontal and base panel.
EFFECT: increase in the manufacturability of the spacecraft during its assembly is achieved.
3 cl, 4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| HULL OF A BLOCK-MODULAR SPACE VEHICLE | 2021 |
|
RU2775790C1 |
| SPACECRAFT ASSEMBLING METHOD | 2017 |
|
RU2658262C1 |
| SPACECRAFT PAYLOAD MODULE ASSEMBLY METHOD | 2021 |
|
RU2771087C1 |
| SPACECRAFT PAYLOAD MODULE CASE | 2022 |
|
RU2780897C1 |
| SPACECRAFT SERVICE SYSTEM MODULE | 2020 |
|
RU2753003C1 |
| SPACECRAFT ASSEMBLY METHOD | 2016 |
|
RU2647404C2 |
| SPACECRAFT PAYLOAD MODULE | 2022 |
|
RU2778178C1 |
| MODULE-CONSTRUCTION SPACE VEHICLE | 1995 |
|
RU2092398C1 |
| SPACECRAFT SERVICE SYSTEMS MODULE HOUSING | 2023 |
|
RU2813378C1 |
| SPACECRAFT ASSEMBLY METHOD | 2021 |
|
RU2764473C1 |
