FIELD: spacecraft.
SUBSTANCE: dashboard of a spacecraft. The technical result is achieved by the instrument panel of the spacecraft, containing the supporting bases, between which a honeycomb core is installed. At the same time, heat pipes are built into the dashboard and through holes are made in which embedded elements with threaded holes are placed. Moreover, in the zone of location of the heat pipe in the dashboard there is a built-in insert of a rectangular section containing a recess for placing and gluing the end part of the heat pipe.
EFFECT: eliminating the violation of the integrity of the heat pipe and increasing the reliability and performance of the spacecraft as a whole.
2 cl, 2 dwg
Title | Year | Author | Number |
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HEAT TRANSFER PANEL OF A SPACE VEHICLE | 2020 |
|
RU2763353C1 |
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RU2648520C2 |
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RU2520811C1 |
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RU2757134C1 |
SPACE VEHICLE | 2011 |
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RU2463219C1 |
SPACE MODULE | 2015 |
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RU2621783C2 |
METHOD OF CONSTRUCTING THE SPACECRAFT | 2018 |
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RU2682891C1 |
ERECTION OF HEAT PIPES IN THREE-PLY PANELS | 2013 |
|
RU2547743C2 |
Authors
Dates
2023-11-21—Published
2023-03-14—Filed