METHOD OF THERMOREGULATION OF SPACECRAFT AND DEVICE FOR ITS DRYING Russian patent published in 2008 - IPC B64G1/50 B64G1/10 

FIELD: heating.

SUBSTANCE: suggested method includes the conduction of heat gain from instruments, installed on middle heat-conducting cellulite panel to the side radiator-oscillator by L-shaped regulating heating tubes (HT). At the same the instrument container of the spacecraft is created by union of two flat-topped heat-conducting cellulite panel blocs, and in each of them it is installed the L-shaped HT. The vaporizers of this HT are made by pairwise connection in the longitudinal direction in the middle cellulite panel. The condensers of HT are made in the side cellulite panel of flat-topped block, which is the side radiator-oscillator. Besides L-shaped HT, for additional heat-conducting from one internal surfaces of the radiator-oscillator and transmission of it to the others radiator-oscillator it is used parallel flat-topped HT. The vaporizers and condensers of the HT are built into additional cellulite panel layer of the proper side radiator-oscillator and orthogonal situated relatively the condensers of L-shaped HT.

EFFECT: it is increased the exactness and safety of the work and it is exceeded the possibility of using the system of thermoregulation.

2 cl, 4 dwg