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10 CFR 50.71(e) - Maritime Administration - U.S. Department of ...

10 CFR 50.71(e) - Maritime Administration - U.S. Department of ...

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Updated Final Safety Analysis Report - (STS-004-002)The main air ejectors are twin-stage, twin-element units with surface type inter- and aftercondensers.Each unit consists <strong>of</strong> two first-stage and two second-stage ejectors mounted on asingle housing, which contains the inter- and after-condensers in separate compartments.Suitable valving was provided to permit the use <strong>of</strong> either or both elements.Air and noncondensible vapors were drawn from the air cooler section <strong>of</strong> the main condenser bythe first-stage nozzle assembly and discharged to the inter-condenser. Any moisture presentwas condensed by the cool condensate that was flowing through the tube side <strong>of</strong> the heatexchanger. The collected liquid was then drained by way <strong>of</strong> the loop seal to the maincondenser. The air and noncondensible vapors were then drawn from the inter-condensersection by the second-stage steam nozzle and discharged to the after-condenser section. Theafter-condenser drains were directed to the atmospheric drain tank while the air andnoncondensible vapors were drawn into the gland seal exhaust system.8.3.2.3. Gland Seal Exhaust SystemAll <strong>of</strong> the main condensate and feedwater system equipment is deactivated, drained, disabledand performs no active function.The main engine turbine rotors were sealed against in-leakage <strong>of</strong> air by a series <strong>of</strong> steam-sealedlabyrinths located at the casing penetrations. The sealing steam was normally supplied at 0.5 to2.0 psig from an auxiliary steam system. The excess steam from the seals was removed bypiping the leak <strong>of</strong>f connections to the after-condenser section <strong>of</strong> the main air ejector. Thecondensed steam then combines with the second-stage nozzle discharge and drains back to theatmospheric drain tank.A gland seal exhaust fan, rated at 200 cfm with <strong>10</strong>0°F air at a static head <strong>of</strong> <strong>10</strong> inches <strong>of</strong> water,took suction from the after-condenser section <strong>of</strong> the main air ejector and discharged to an aircooled, shell-and-tube gland exhaust condenser. Any remaining entrained moisture wascondensed and drained to the low-pressure drain system. The combined air and noncondensiblevapors were discharged to an engine room exhaust system.The gland seal exhaust system effluent was continuously sampled by the radiation monitoringsystem for radioactive particulate daughter products <strong>of</strong> fission gases. This detectorarrangement, operating in conjunction with secondary system water sampling, served as anearly warning for the presence <strong>of</strong> a primary-to-secondary system leak.8.4 Emergency Propulsion SystemAll <strong>of</strong> the emergency propulsion system equipment is deactivated, disabled and performs no activefunction. Emergency Propulsion was provided by the 440 v-ac, 750 HP auxiliary propulsion motor.8.5 Electrical Power SystemsThe following portions <strong>of</strong> the electrical power system equipment are deactivated, disabled and perform noactive function:Ship’s Service Turbine generators;Auxiliary diesel generators;Motor generator sets;Battery backup systems; and,Emergency diesel generator.Rev. VI 77

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