FIELD: astronautics.
SUBSTANCE: invention relates to the space equipment. In the method, the spacecraft contains two telescopes mounted on the support nodes of the upper belt of the truss, and a module of service systems. Said upper truss belt contains six support nodes, and the lower one contains eight. Said four support nodes of the upper belt of the truss are aligned with the vertices of the deltoid, and the two are located symmetrically relative to its long diagonal and aligned with the sides of the deltoid. Said case of the utility systems module is made in the form of a regular straight octahedral prism, along the edges of which the longitudinal posts are missing. Further, the length of the larger diagonal of the deltoid is chosen longer, and the length of the short diagonal is chosen as the smaller overall transverse size of the utility systems module. And the supporting nodes of the lower belt of the truss are rigidly fixed on the longitudinal posts of the body, and their upper ends are tightened with rods of a flat truss.
EFFECT: technical result of the invention is to ensure the strength and rigidity of the power circuit of the spacecraft, the possibility of placing two telescopes with different weights on board.
10 cl, 14 dwg
Title | Year | Author | Number |
---|---|---|---|
SERVICE SYSTEM MODULE | 2015 |
|
RU2621221C1 |
SPACECRAFT, ITS PAYLOAD MODULE AND SERVICE SYSTEM MODULE | 2016 |
|
RU2617162C1 |
SERVICE SYSTEM MODULE | 2015 |
|
RU2617018C1 |
SPACECRAFT FOR DELIVERING PAYLOAD TO SPACE BODY WITH SMALL GRAVITATIONAL FIELD | 2020 |
|
RU2758656C1 |
TRANSITIONAL TRUSS | 2021 |
|
RU2779010C1 |
DEVICE FOR GROUP LAUNCH OF SATELLITES AND REINFORCED FRAME | 2020 |
|
RU2725824C1 |
ADAPTER FOR WAY LOOSE OF USEFUL LOAD | 2016 |
|
RU2624959C1 |
TRANSFER COMPARTMENT OF CARRIER ROCKET (VERSIONS) | 2015 |
|
RU2603872C1 |
DEVICE FOR GROUP LAUNCHING OF SATELLITES | 2019 |
|
RU2724000C1 |
GANTRY CRANE | 0 |
|
SU887436A1 |
Authors
Dates
2018-11-26—Published
2017-10-11—Filed