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DESIGN REQUIREMENTS AND SYSTEMS COMPARISONS
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45-day mission absorption refrigeration approximately argon battery Brayton cycle Brayton system btu/hr cabin heat carbon dioxide closed loop compressor Condensate Pump configuration coolant Cylinder 4 Dia dormant period efficiency electrical power requirements fluid fuel cell heat exchanger heat input Heat Leakage heat load heat source heat transfer hydrogen hydrogen-oxygen engine Hypergolic Integrated Brayton integrated system internal combustion engine isotope source kw-hr liquid lunar roving vehicle lunar surface maximum molecular sieve nonintegrated system operating oxide OXYGEN RECOVERY peak pounds power conditioning loss power level power profile power system weight pressure drop propellant pump power pyrolysis radiator area radiator design Rankine cycle Rankine system Reference regeneration Sabatier reactor sensible heat shield shown in Figure support system TABLE thermal control thermal energy thermal integration thermal power trailer module turbine Urine utilized vapor fin radiator vapor tube Wash Water waste heat water recovery watts