FIELD: cosmonautics.
SUBSTANCE: invention relates to space industry and is intended for connection of two power structures of spacecraft (SC), in particular, for docking of power mesh structure (PMS) of SC with metal cylindrical body of SC. Lock for docking of power mesh structure (PMS) with metal cylindrical body of spacecraft contains projections and nuts fixing position of lock. Lock contains a rocker connected by means of axes with two pins. One pin is installed in the hole on the inner projection of the metal cylindrical body. Second pin is installed in the cutout on the outer projection of the metal cylindrical body. Pins are fixed with nuts. Spherical support and a spherical washer are installed in front of the nut of the external pin. Flat washers are installed in front of the inner pin nuts.
EFFECT: provision of reliability of connection of PMS with metal cylindrical body.
5 cl, 5 dwg
Title | Year | Author | Number |
---|---|---|---|
ASSEMBLY FOR DOCKING OF SPACECRAFT LOAD CARRYING STRUCTURE (VERSIONS) | 2019 |
|
RU2729909C1 |
REINFORCEMENT UNIT FOR FRAME OF FORCE LATTICE CONSTRUCTION OF HOUSING FROM POLYMER COMPOSITE MATERIALS (VERSIONS) | 2019 |
|
RU2733309C1 |
METHOD FOR SECURING AND DETACHING PAYLOAD | 2021 |
|
RU2769847C1 |
PAYLOAD ATTACHMENT AND SEPARATION SYSTEM | 2021 |
|
RU2764879C1 |
CARRIER ROCKET LARGE-SIZE DETACHABLE NOSE CONE | 2010 |
|
RU2424953C1 |
ADJUSTMENT CONNECTING DEVICE | 2014 |
|
RU2605666C2 |
METHOD FOR ASSEMBLING XENON HIGH PRESSURE TANK WITH CABLE FASTENING SYSTEM | 2022 |
|
RU2793771C1 |
UNIVERSAL MOUNTING INTERFACE FOR INTERROJUSTATION OF EQUIPMENT WITH CABLE FASTENING SYSTEM | 2018 |
|
RU2689892C1 |
CARRIER ROCKET DETACHABLE NOSE CONE | 2010 |
|
RU2428359C1 |
ADJUSTABLE SECURING ASSEMBLY | 2013 |
|
RU2559370C2 |
Authors
Dates
2024-09-19—Published
2024-04-15—Filed