FIELD: discharge of thermal power released during operation of space power plant into space. SUBSTANCE: device includes cylindrical or taper shell to which tubular members are welded; heat transfer agent is pumped through these tubular members. Tubular members are so profiled that cross section of each member is bounded by arc of larger half of circle and chord. Flat surfaces of tubular members are connected with inner surface of load-bearing shell over entire length but for sections adjoining headers. EFFECT: reduction of mass of power plant with no reduction of heat-conducting capacity of cooler-radiator. 2 dwg
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