“…Interest in prospective candidate Li–S and Li–O 2 EES technologies is increasing because they offer the interconversion of chemical and electrical energy on a relatively short time scale, theoretically with higher efficiency than that of a heat engine and without releasing polluting gas emissions to the environment (Bruce et al, 2012; Li et al, 2015). However, high-energy density electrochemical rechargeable batteries should also be safe, inexpensive, nontoxic, and reliable through thousands of charge–discharge cycles to deliver long-term discharge capacities above 1,000 mAh/g and specific energy densities above 600 W h/kg required for emerging practical applications, e.g., in high-endurance unmanned aerial vehicle systems (UAVs) and electric vehicles capable of traveling over 500 km on a single charge (Ji et al, 2009; Oleshko et al, 2009 a , 2015 a , 2015 b ). Specifically, light-weight rechargeable Li–S batteries based on the Li/S redox couple generating ~2.2 V with respect to Li + /Li° have the highest theoretical specific capacity of 1,672 mAh/g of active material among all solid elemental redox couples and a theoretical specific energy of 2,567 W h/kg, assuming a complete two-electron reaction (Peled et al, 1989; Marmorstein et al, 2000): …”