HEAT TRANSFER PANEL OF SPACE VEHICLE Russian patent published in 2014 - IPC F28D15/02 

FIELD: heating.

SUBSTANCE: heat transfer panel can be used in temperature control systems of space vehicles (SV) for providing of temperature conditions of the equipment installed in earth satellites, interplanetary stations, landers and other space objects. SV heat transfer panel contains metal skin and built-in heat tubes. The panel is designed as sectional and consists of rigidly connected with each other separate hollow sections with heat tubes. Each section of the panel, including heat tubes, is designed as a uniform monolithic structure.

EFFECT: panel allows to improve the efficiency of heat contact between the cooled equipment and built-in heat tubes, unify the structure components, improve reliability and life of the panel, minimize pollution of SV internal atmosphere at the expense of avoidance of glue from used materials, and significantly simplify the technology of fabrication of instrument panel, which combines in itself heat and strength functions.

11 cl, 7 dwg