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Kasilov
77-30569/253502 Radiator of the space power plant
Engineering Education # 10, October 2011 It is considered a method for calculating the radiator of the closed loop space power plant. It gives the calculations of the radiators of various designs, analyses the influence of geometrical parameters of the radiating ribs on the weight and dimensions of the device, gives the results of calculation. It was considered the radiator circuit with an intermediate heat transfer medium, given analyses of advantages and disadvantages of this scheme. It is proposed a structure that has no hinges that completely eliminates the leakage of coolant during the deployment of the systems in space in running condition
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