FIELD: transportation.
SUBSTANCE: satellite consists of two modules: payload module and support system module, and their devices are fitted on honeycomb panels with built-in channels for circulating heat carrier under the devices. Radiators, with channels for circulating heat carrier, are placed in perpendicular planes to the axis +Z (-Z) of the spacecraft. Most of the devices of the payload module are fitted on extra panels with built-in channels for circulating heat carrier by putting them inside the provided free space between panels of the support system module. Opening-up extra radiator panels with built-in channels on the section of raising the spacecraft to the working orbit are folded parallel to the panels of the support system module, placed in planes perpendicular to the axis Y (-Y) of the spacecraft.
EFFECT: more reliable operation of devices of a spacecraft.
2 cl, 6 dwg
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SPACECRAFT HEAT REGULATION SYSTEM | 2014 |
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SPACECRAFT TEMPERATURE CONTROL SYSTEM | 2007 |
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SYSTEM OF SPACECRAFT THERMAL CONTROL | 2008 |
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Authors
Dates
2009-02-20—Published
2007-03-05—Filed