FIELD: nuclear plants. SUBSTANCE: proposed system has bypass mainline with control valve connected between inlet and outlet of recuperator heat sensing duct which permits changing of temperature of propulsive mass in nuclear reactor cooling ducts at starting and cutting off of nuclear rocket engine and maintaining of required thermal conditions of inlet sections of heat generating assemblies and retarder at reduced heat power conditions. EFFECT: enhanced reliability of nuclear rocket engine at transient conditions. 1 dwg
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