SPACECRAFT Russian patent published in 2015 - IPC B64G1/22 B64G1/50 

FIELD: aircraft engineering.

SUBSTANCE: spacecraft comprises target hardware module, service systems module with power supply incorporates solar cells, ACS module, storage batteries, thermal control system integrating control unit, hydraulic units, panes of suspended composed of separate assembly units with thermal control end heat exchanger with fluid heart carrier and heat pipe, thermal boards with fluid heat carrier, heat tube with flat shelves and heat lines with hydraulic valves. Thermal control end heat exchanger consists of units tightly connected by inlets-outlets composed of hollow body of revolution and solid coil with central part shaped to truncated cone. Material and sizes of heat pipe and thermal control end heat exchanges, spacing between heat pipes are selected subject to maximum transferred thermal power transferred from heat carrier to heat pipe and minimum vulnerability to meter and man-made particles, and thermal control end heat exchanger surface area.

EFFECT: improved multifunctionality.

3 dwg