FIELD: space technology.
SUBSTANCE: invention relates to field of space technology, and more specifically to the assembly of spacecraft (SC). Method is proposed for connecting the base and instrument panels of the spacecraft payload module using discrete attachment points, in which the attachment points are made in form of lever mechanisms. The mechanisms rigidly connect the panels to each other and link them using a stretched cable. With the free end the cable is connected to actuator. With help of actuator, the tension of cable is weakened, as a result lever mechanisms ensure removal of mechanical connections between panels in plane of the base panel.
EFFECT: increase in SC work efficiency is achieved.
1 cl, 5 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| BODY OF A BLOCK-MODULAR SPACECRAFT AND THE METHOD FOR ITS ASSEMBLY | 2021 |
|
RU2771471C1 |
| SPACECRAFT PAYLOAD MODULE CASE | 2022 |
|
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|
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| SPACE PLATFORM | 2016 |
|
RU2688630C2 |
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|
RU2778178C1 |
| MULTIPLE RETENTION AND RELEASE APPARATUS FOR A SPACE VEHICLE AND METHODS FOR RELEASING A SPACE VEHICLE FROM THE DELIVERY APPARATUS OF THE LAUNCH VEHICLE AND FOR INSTALLING THE MULTIPLE RETENTION AND RELEASE APPARATUS FOR A SPACE VEHICLE | 2019 |
|
RU2787984C1 |
| SPACECRAFT ASSEMBLY METHOD | 2016 |
|
RU2647404C2 |
| SPACECRAFT PAYLOAD MODULE | 2019 |
|
RU2729148C1 |
| HULL OF A BLOCK-MODULAR SPACE VEHICLE | 2021 |
|
RU2775790C1 |
| SPACE PLATFORM | 2016 |
|
RU2648520C2 |
