FIELD: transport.
SUBSTANCE: invention relates aerospace engineering. Proposed method comprises radiator pumping and its filling with working body (heat carrier) at differential pressure. Note here that, on the earth, radiator is disconnected from heat control system and filled with preset-pressure inert gas. After placing in orbit, radiator tightness is checked up and inert gas is released outboard. Then, radiator is connected to heat control system. Radiator may be placed in orbit incorporated with module, either arranged therein or separately, inside manned spaceship. Said radiator may be transferred (separately or together with module) from spaceship compartment, for example, in docking to other space objects.
EFFECT: higher safety of radiator operation.
1 dwg
