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12. Bypass diode failure—Bypass diodes used to overcome cell mismatching
                            problems can themselves fail, usually due to overheating and often due to
                            undersizing (Durand, 1994). The problem is minimised if junction
                            temperatures are kept below 128°C.

                         13. Encapsulant failure—UV absorbers and other encapsulant stabilisers ensure
                            a long life for module encapsulating materials. However, slow depletion, by
                            leaching and diffusion, does occur and, once concentrations fall below a
                            critical level, rapid degradation of the encapsulant materials occurs. In
                            particular, browning of the EVA layer, accompanied by a build-up of acetic
                            acid, has caused gradual reductions in the output of some arrays, especially
                            those in concentrating systems (Wenger et al., 1991; Czanderna & Pern,
                            1996; King et al., 2000), although recent improvements in EVA
                            photostability have reduced this problem.


                     5.12  EMBODIED ENERGY AND LIFE CYCLE ISSUES
                     Early solar cells required significant levels of material use and processing energy.
                     This raised the issue of net energy production by photovoltaics. Modern commercial
                     products are higher in efficiency than the early cells, production techniques minimise
                     material use and wastage, while energy use has become more efficient, so that there is
                     no longer any question that photovoltaic cells pay back their manufacturing energy in
                     the early years of their operation. Effort is now being directed to developing
                     manufacturing methods that facilitate module recycling (Wambach, 2004; Arai et al.,
                     2004).
                     A number of methods, including process analyses or input-output techniques, are
                     used to calculate and report on the energy used to manufacture components and
                     modules, which is referred to as the embodied energy of manufacture (E man ). This is
                     the primary energy requirement during module manufacture, including materials
                     mining.
                     Life cycle analysis (LCA) techniques (sometimes known as cradle-to-grave analyses)
                     are also used to follow both the materials and the energy flow through manufacturing,
                     operation and end-of-life. Methodologies used are covered under the International
                     Standards Organisation Life Cycle Assessment standard ISO 14040. For energy use,
                     E input  can be defined as the sum of primary energy requirements for manufacturing
                     (E man ), transport (E trans ), installation (E inst ), operation (E use ) and decommissioning
                     (E decomm ) (Kato, 2000)

                                       E       E     E      E     E     E          (5.4)
                                         input  man  trans  inst  use  decomm
                     For each year the PV module is in operation, it will displace a certain amount of
                     energy that would otherwise have been used for electricity generation. This is referred
                     to as E gen  and will vary with site and fuel displaced. The term energy payback time
                     (EPT or EPBT) refers to the time taken for the input energy to be repaid by PV
                     generation. Hence

                                                          E input
                                                    EPT                            (5.5)
                                                           E
                                                            gen




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