FIELD: satellite technology.
SUBSTANCE: group of inventions relates to device (20) for deployment of first (11) and second (12) tools (for example, antennas), as well as to a satellite, on which it is installed. The device contains main lever (14) with main engine (15) of lever rotation relatively to surface (81) of structure (80), connected to both tools (11, 12). Tool (12) is equipped with secondary engine (16) for movement relatively to main lever (14). These means provide transfer of tools (11, 12) from a folded configuration on surface (81) to a working configuration and back.
EFFECT: achievement of compactness of a deployment device, reduction in a number of auxiliary elements and drives, and, thereby, simplification and reduction in weight of the device.
9 cl, 9 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| SATELLITE DOCKING SYSTEM AND METHOD | 2015 |
|
RU2750349C2 |
| DEPLOYABLE ANTENNA ASSEMBLY | 2019 |
|
RU2795105C1 |
| DEVICE FOR DEPLOYMENT AND FOLDING OF FLEXIBLE STRUCTURE, FLEXIBLE DEPLOYABLE STRUCTURE AND SATELLITE, EQUIPPED WITH SUCH DEVICE | 2013 |
|
RU2641398C2 |
| COMPONENT DEVELOPMENT SYSTEM | 2014 |
|
RU2678296C2 |
| RECONFIGURABLE RADIATING ANTENNA ARRAY | 2007 |
|
RU2406189C1 |
| DEPLOYABLE SATELLITE ANTENNA LARGE-SIZE REFLECTOR | 2013 |
|
RU2607837C2 |
| STACKABLE DISC-SHAPED SATELLITE | 2017 |
|
RU2736893C2 |
| SYSTEM AND METHOD FOR ASSEMBLY OF FOLDED VALVE INTRODUCED THROUGH SKIN | 2013 |
|
RU2609461C2 |
| FOLDING RADIO FREQUENCY MEMBRANE ANTENNA | 2017 |
|
RU2748242C2 |
| TEMPORARY VALVE AND VALVE FILTER | 2014 |
|
RU2634683C2 |
