FIELD: astronautics.
SUBSTANCE: group of inventions relates to external deployable components of a spacecraft, for example, solar panels or antennae, mounted primarily on small satellites. Apparatus comprises a group of panels folded tightly to each other on a side of a spacecraft, a group of flexible members connected to the panels, and an interface system associated with said groups. Interface system is configured to move the group of panels from the folded configuration to a deployed configuration when the group of flexible members is extended from the spacecraft.
EFFECT: technical result is aimed at increasing the compactness of deployable spacecraft components in a folded state.
12 cl, 38 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| STACKABLE DISC-SHAPED SATELLITE | 2017 |
|
RU2736893C2 |
| DEPLOYABLE ANTENNA ASSEMBLY | 2019 |
|
RU2795105C1 |
| FOLDING RADIO FREQUENCY MEMBRANE ANTENNA | 2017 |
|
RU2748242C2 |
| PORTABLE GROUND-BASED DIFFERENTIAL CORRECTION SYSTEM | 2015 |
|
RU2684134C2 |
| SPACE MIRROR AND METHOD OF ITS DEVELOPMENT IN SPACE (VERSIONS) | 2009 |
|
RU2424162C2 |
| HITLESS REARRANGEMENT OF A SATELLITE-HOSTED SWITCH VIA PROPAGATED SYNCHRONIZATION | 2015 |
|
RU2684734C2 |
| COMPENSATION OF THE NON-IDEAL SURFACE OF THE REFLECTOR IN THE SATELLITE COMMUNICATION SYSTEM | 2014 |
|
RU2647559C2 |
| IMPROVEMENT OF REMOTE-PROBING OR REMOTE- COMMUNICATION SPACE VEHICLES | 1997 |
|
RU2199803C2 |
| SATELLITE DOCKING SYSTEM AND METHOD | 2015 |
|
RU2750349C2 |
| THERMAL CONTROL SYSTEM FOR CONTROLLING TEMPERATURE OF REFLECTING SURFACE HAVING ARRAY OF SOLAR ENERGY CONCENTRATORS | 2017 |
|
RU2754718C2 |
