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NASA Redox Storage System Development Project

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NASA Redox Storage System Development Project ( nasa-redox-storage-system-development-project )

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- I . 8 0 Polarity 0 Standard. after 20 40 60 80 100 120 140 Currentdensity, m ~ l c m ~ 1- Y285-64C W285-9039 U285-87 W285-89 W285-99 (7mii) W285-99 (4mi1) MT306-34 1 Type ( Sourcc 1 Figure 24 - Effed of complete polarity reversal on performance. BismuthCatalyst:ML-21membrane: stateofcharge. 50per- cent: temperature, 65 OC; mixed r-ctants: bismuth salt i n each reactant 70I f u For (a) Coulombicefficiency. 60 s s 20 40 60 80 100 1M 140 160 Current density, m ~ l c m ~ (bl Energyefficiency. Figure 25 - Effect of current densi2on working cell efficiency for developn~entaml embranes. current cycles: temperature. 65 C: mixed reactants. CPS-1 TABLE V. - EFFECT OF TEMPERATURE ON SELECTIVITY OF MEMBRANES FOR ELEVATED-TEMPERATURE OPERATION WITH MIXED REACTANTS 0 w7U-39 0 W285-99CI mill v W285-99 (4 mill 0 ML-2l D 1155-2l4-45 Cation Temperature, *C 2210 --- 35 Asahi 60 RA I 770 180 200 Constant-

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