FIELD: astronautics.
SUBSTANCE: group of inventions relates to thermal control means, in particular, powerful space power plants. Heat release device, in the first version, contains heat-radiating elements in the form of ball-shaped containers, which are serially connected (pipes) for the gaseous heat carrier flow. In the second version, a deflector is installed inside each reservoir, forming a cavity for the flow of gaseous heat carrier with the inner surface of its wall.
EFFECT: simplification of heat release device design, reduction of its weight and dimensions.
6 cl, 4 dwg, 1 tbl
| Title | Year | Author | Number |
|---|---|---|---|
| SPACE POWER PLANT WITH MACHINE ENERGY CONVERSION | 2017 |
|
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| SPACE POWER PLANT WITH MACHINE ENERGY CONVERSION | 2015 |
|
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|
RU2583191C1 |
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|
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|
RU2802305C1 |
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|
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| REFRIGERATOR-EMITTER PANEL | 2015 |
|
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| EXTRA-TERRESTRIAL POWER PLANT WITH COMPUTER-AIDED ENERGY CONVERSION | 2012 |
|
RU2508460C1 |
| METHOD FOR ACCUMULATING AND GENERATING ENERGY AND APPARATUS FOR IMPLEMENTATION THEREOF | 2020 |
|
RU2783246C2 |
| SPACECRAFT NUCLEAR PROPULSION SYSTEM | 2013 |
|
RU2533672C1 |
