FIELD: serviced satellites.
SUBSTANCE: group of inventions relates to the design and use of a serviced satellite (SS) (100) equipped with at least two maneuvering engines (101, 103), one controller and two docking levers (108) with end grips (109) rotatable relative to the body (110). The grips are designed to engage with a docking frame (not shown) protruding above the surface of the serviced orbital satellite (OS). Each lever is independently controlled by a controller that coordinates the movement of the levers and the gripping of the OS, as well as starting the maneuvering engines (101, 103) to move the OS by means of the forces applied through the specified docking frame. For precision orientation of the SS, an electric rocket motor (107) on a rod (113) can be provided.
EFFECT: ensuring high compatibility of the SS with a variety of operating systems and other objects (including space debris) that have a docking frame as a typical common element.
25 cl, 39 dwg
| Title | Year | Author | Number |
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|
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| SERVING SATELLITE FOR ORBITAL SERVICES USING VARIABLE ENGINE CONTROL | 2022 |
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|
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| SPACECRAFT SERVICING DEVICES AND CORRESPONDING NODES, SYSTEMS AND METHODS | 2018 |
|
RU2765021C2 |
| SPACE SYSTEM FOR RECYCLING LARGE-SIZE SPACE DEBRIS | 2018 |
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| DEVICE FOR DELIVERY OF TOURISTS FROM NEAR-MOON ORBIT TO SURFACE OF MOON AND SUBSEQUENT RETURN TO GROUND | 2019 |
|
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| SPACE INFRASTRUCTURE FOR MAINTENANCE OF SPACE OBJECTS ON GEOSTATIONARY AND LOWER ORBITS, AS WELL AS METHOD FOR MAINTENANCE OF SPACE OBJECTS BY MEANS OF THIS INFRASTRUCTURE | 2022 |
|
RU2776887C1 |
| SPACE HEAD FOR GROUP LAUNCH OF SATELLITES | 2010 |
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RU2428358C1 |
